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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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264 Waves<br />

r/a<br />

5<br />

4<br />

3<br />

2<br />

1<br />

0 0 2 4 6 8<br />

arise on the boundary at in®nity.y This is discussed by Bettess. 40 <strong>The</strong> terms can be<br />

evaluated, but they are not symmetrical (or hermitian), and therefore impose a<br />

change of solution technique. An alternative, which eliminates the terms at in®nity,<br />

was proposed by Astley et al. 48 In this a `geometrical factor' is included in the<br />

weighting function, which then takes the form<br />

N i…r; † r i<br />

r<br />

3<br />

e ik…r ÿ r i†<br />

…8:43†<br />

It has been shown that this form of weighting functions gives very good results. Such<br />

wave envelope in®nite elements have been further developed by Coyette, Cremers and<br />

Fyfe. 49;50 <strong>The</strong>se elements have incorporated a more general mapping than that in the<br />

original <strong>Zienkiewicz</strong> et al. mapped in®nite wave element. Cremers and Fyfe allow the<br />

mapping to vary in the local and directions.<br />

8.14 Accuracy of in®nite elements<br />

<strong>The</strong> use of a complex conjugate weighting in the wave envelope in®nite elements means<br />

that the original variational statement, Eq. (8.22), must be changed to allow the use of<br />

the di€erent weighting function. This gives rise to a number of issues relating to the<br />

nature of the weighted residual statement and the existence of various terms. <strong>The</strong>se<br />

issues were touched on by Bettess, 40 but have been subsequently subjected to more<br />

detailed study. Gerdes and Demkowitz, 55;56 analysed the wave envelope elements,<br />

and subsequently the wave in®nite elements. 57 Some of this work is restricted to<br />

z/a<br />

Incident mode number = 1<br />

Reduced frequency ka == 11<br />

Spiral mode number m φ = 8<br />

Plane wavelength<br />

Conventional FEM<br />

Wave envelope FEM<br />

Fig. 8.9 Computed acoustical pressure contours for a hyperbolic duct … 0 ˆ 708, ka ˆ 11, m ˆ 8†. Conventional<br />

and wave envelope element solutions, Astley. 20<br />

y Some writers, particularly mathematicians, prefer to call the usual wave in®nite elements, unconjugated<br />

in®nite elements, and the Astley type wave envelope in®nite elements, conjugated in®nite elements.

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