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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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spherical scatterers. Other analysis is carried out by Shirron and BabusÏ ka, 58;59 who<br />

reveal a somewhat paradoxical result. <strong>The</strong> usual in®nite elements give better results<br />

in the ®nite element mesh, but worse results in the in®nite elements themselves. But<br />

the wave envelope elements give worse results in the ®nite elements, and better results<br />

in the far ®eld. This result, which is ascribed to ill-conditioning, does seem to be<br />

counterintuitive. Astley 41 and Gerdes 42 have also surveyed current formulations and<br />

accuracies.<br />

8.15 Transient problems<br />

Recently Astley 60ÿ63 has extended his wave envelope in®nite elements, using the prolate<br />

and oblate spheroidal coordinates adopted by Burnett and Holford, 51ÿ53 and has<br />

shown that they give accurate solutions to a range of periodic wave problems. With<br />

the geometric factor of Astley, which reduces the weighting function and eliminates<br />

the surface integrals at in®nity, the sti€ness, K, damping, C, and mass M matrices<br />

of the wave envelope in®nite element become well de®ned and frequency independent,<br />

although unsymmetric. This makes it possible to apply such elements to unbounded<br />

transient wave problems. Figure 8.10 shows the transient response of a dipole.<br />

More results from the application of in®nite elements to transient problems are<br />

given by Cipolla and Butler, 64 who created a transient version of the Burnett in®nite<br />

element. <strong>The</strong>re appear to be more di culties with such elements than with the wave<br />

envelope elements, and a consensus that the latter are better for transient problems<br />

seems to be emerging. Dampers and boundary integrals can also be used for transient<br />

problems. Space is not available to survey these ®elds, but the reader is directed,<br />

again, to Givoli 29 and Geers. 30 One set of interesting results was obtained using<br />

transient dampers by Thompson and Pinsky. 65<br />

Dimensionless acoustic pressure<br />

1.5<br />

1.0<br />

0.5<br />

0<br />

–0.5<br />

–1.0<br />

P(A)<br />

P(B)<br />

P(C)<br />

–1.5 0 0.5 1.0 1.5 2.0 2.5 <strong>3.</strong>0<br />

Fig. 8.10 Transient response of a dipole, Astley. 63<br />

Dimensionless time T (= tD/c)<br />

Transient problems 265

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