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Zienkiewicz O.C., Taylor R.L. Vol. 3. The finite - tiera.ru

Zienkiewicz O.C., Taylor R.L. Vol. 3. The finite - tiera.ru

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arising from integrating by parts the viscous contribution. Since the residual on the<br />

boundaries can be neglected, other boundary contributions from the stabilizing terms<br />

are negligible. Note from Eq. (2.91) that the whole residual appears in the stabilizing<br />

term. However, we have omitted higher-order terms in the above equation for clarity.<br />

As mentioned in Chapter 1, it is convenient to use matrix notation when the ®nite<br />

element formulation is carried out. We start here from Eq. (1.7) of Chapter 1 and we<br />

repeat the deviatoric stress and strain relations below<br />

_" kk<br />

ij ˆ 2 _" ij ÿ ij<br />

…3:33†<br />

3<br />

where the quantity in brackets is the deviatoric strain. In the above<br />

and<br />

_" ij ˆ 1<br />

2<br />

@ui ‡<br />

@xj @uj @xi …3:34†<br />

_" ii ˆ @ui …3:35†<br />

@xi We now de®ne the strain in three dimensions by a six-component vector (or in two<br />

dimensions by a three-component vector) as given below (dropping the dot for<br />

simplicity)<br />

e ˆ ‰ " 11 " 22 " 33 2" 12 2" 23 2" 31 Š T ˆ " x " y " z 2" xy 2" xz 2" zx<br />

T<br />

…3:36†<br />

with a matrix m de®ned as<br />

m ˆ ‰ 1 1 1 0 0 0Š<br />

T<br />

We ®nd that the volumetric strain is<br />

…3:37†<br />

" v ˆ " 11 ‡ " 22 ‡ " 33 ˆ " x ‡ " y ‡ " z ˆ m T e …3:38†<br />

<strong>The</strong> deviatoric strain can now be written simply as (see Eq. <strong>3.</strong>33)<br />

e d ˆ e ÿ 1<br />

3 m" v ˆ I ÿ 1<br />

3 mmT<br />

ÿ<br />

e ˆ Ide …3:39†<br />

where<br />

Id ˆ I ÿ 1<br />

3 mmT<br />

ÿ<br />

…3:40†<br />

and thus<br />

Id ˆ 1<br />

2<br />

2 ÿ1 ÿ1 0 0<br />

3<br />

0<br />

6 ÿ1<br />

6 ÿ1<br />

6<br />

3 6 0<br />

6<br />

4 0<br />

2<br />

ÿ1<br />

0<br />

0<br />

ÿ1<br />

2<br />

0<br />

0<br />

0<br />

0<br />

3<br />

0<br />

0<br />

0<br />

0<br />

3<br />

0 7<br />

0 7<br />

0 7<br />

05<br />

…3:41†<br />

0 0 0 0 0 3<br />

If stresses are similarly written in vectorial form as<br />

r ˆ ‰ 11 22 33 12 23 31 Š T<br />

Characteristic-based split (CBS) algorithm 71<br />

…3:42†<br />

where of course 11 is identically equal to x and is also equal to 11 ÿ p with similar<br />

expressions for y and z, while 12 is identical to 12, etc.

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