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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

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

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196 Compressible high-speed gas ¯ow<br />

dealt with from time to time and here we illustrate the process on three examples. <strong>The</strong><br />

®rst one concerns an exploding pressure vessel 73 as a two-dimensional model as<br />

shown in Fig. 6.17. Here of course adaptivity had to be used and the mesh is regenerated<br />

every few steps to reproduce the transient motion of the shock front.<br />

A similar computation is shown in Fig. 6.18 where a diagrammatic form of a shuttle<br />

launch is modelled again as a two-dimensional problem. 73 Of course this twodimensional<br />

model is purely imaginary but it is useful for showing the general<br />

NE = 7870<br />

NP = 4130<br />

NE = 7377<br />

NP = 3867<br />

NE = 6847<br />

NP = 3580<br />

NE = 8459<br />

NP = 4379<br />

Fig. 6.18 A transient problem with adaptive remeshing. 73 Model of the separation of shuttle and rocket.<br />

Mach 2, angle of attack ÿ48, initial mesh 4130 nodes.

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