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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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x 2<br />

1.0<br />

0.8<br />

0.6<br />

0.4<br />

0.4<br />

0.2<br />

'CBS'<br />

0.2<br />

'Ghia'<br />

'CBS'<br />

0<br />

–0.4 –0.2 0 0.2 0.4 0.6 0.8 1.0<br />

0<br />

–0.4 –0.2 0 0.2 0.4 0.6 0.8 1.0<br />

u 1<br />

u 1<br />

(a) Stokes flow, viscosity 1<br />

(b) Re = 400<br />

x 2<br />

1.0<br />

0.8<br />

0.6<br />

Use of the CBS algorithm for incompressible or nearly incompressible ¯ows 99<br />

smaller number of iterations is required to reach steady state and gives an accurate<br />

solution even at the higher Reynolds numbers. Here a solution for a Reynolds<br />

number of 10 000 is given in Fig. 4.9.<br />

4.<strong>3.</strong>3 Fully explicit mode and arti®cial compressibility<br />

x 2<br />

x 2<br />

0.4<br />

0.4<br />

0.2<br />

'Ghia'<br />

'CBS'<br />

0.2<br />

'Ghia'<br />

'CBS'<br />

0<br />

–0.4 –0.2 0 0.2 0.4 0.6 0.8 1.0<br />

0<br />

–0.6 –0.4 –0.2 0 0.2 0.4 0.6 0.8 1.0<br />

u 1<br />

u 1<br />

(c) Re = 1000<br />

(d) Re = 5000<br />

Fig. 4.4 Lid-driven cavity. u 1: velocity distribution along vertical centre-line for different Reynolds numbers<br />

(semi-implicit form).<br />

It is of course impossible to model fully incompressible problems explicitly as the<br />

length of the stable time step is simply zero. However, the reader will observe that<br />

for steady-state solutions the ®rst term of the continuity equation, i.e.<br />

1<br />

c2 @p<br />

…4:20†<br />

@t<br />

does not enter the steady-state calculations and we could thus use any reasonably<br />

large value of c 2 instead of in®nity. This arti®ce has been used with some success<br />

and the solution for a cavity is reported in reference 9 so we do not repeat the results<br />

here.<br />

1.0<br />

0.8<br />

0.6<br />

1.0<br />

0.8<br />

0.6

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