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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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M = 3<br />

r = 1<br />

u 1 = 1<br />

u 2 = 0<br />

5<br />

1<br />

Adaptive re®nement and shock capture in Euler problems 185<br />

10<br />

(a) (b)<br />

(c) (d)<br />

Fig. 6.9 Supersonic ¯ow past a full cylinder. 56 M ˆ 3, (a) geometry and boundary conditions, (b) adapted<br />

mesh, nodes: 12651, elements: 24 979, (c) Mach contours using second derivative shockcapture and (d)<br />

Mach contours using anisotropic shockcapture.

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