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Second Computational Aeroacoustics (CAA) Workshop on ...

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The soluti<strong>on</strong> for pressure, p, can be written as<br />

Substituti<strong>on</strong> of (10) into (7), (9) gives the problem for _(x,y)<br />

__OP=0 at z_+y2=0.25 (9) _;<br />

p(x,y,t) = !m(_(x,g)e -i_') (10)<br />

02D 02P -ia;e -b[(x-=')_+y_] (11)<br />

Ox---- 7 + _ + _2i_ =<br />

015 _ g2<br />

On -0 at x _+ =0.25 (12)<br />

radiati<strong>on</strong> boundary c<strong>on</strong>diti<strong>on</strong>s as x, y --4 oc (13)<br />

(11) is a n<strong>on</strong>-homogeneous I-Ielmholtz equati<strong>on</strong>. The problem (11) - (13) can be solved by the<br />

method of superpositi<strong>on</strong>. Let<br />

_(_,y) = pi(x,_) + p_(x,y) (14)<br />

where pi is the incident wave generated by the source and p_ is the wave reflected off the cylin-<br />

der. pi satisfies<br />

-4- w2pi --" -iwe -b[(_-_')_ +y_]<br />

and the outgoing wave c<strong>on</strong>diti<strong>on</strong>. When pi is found the problem for p_ becomes<br />

02pr 02pr<br />

Ox--- 7- + _ + W2p_ = 0 (16)<br />

Op____Z__ = Opi<br />

On On<br />

(15)<br />

at x 2 + g2 = 0.25 (17)<br />

To solve for p,(z, y) we use polar coordinates (r=, 0_) with the origin at x = z=, y = 0; thus the<br />

soluti<strong>on</strong> is independent of 0_. (16) reduces to the n<strong>on</strong>-homogeneous Bessel equati<strong>on</strong><br />

with boundary c<strong>on</strong>diti<strong>on</strong>s<br />

d2Pi d- 1 dpi -4-wZpi --iwe -br_ (18)<br />

dr] r s dr=<br />

pi(r=) is bounded at r= = 0 (19)<br />

10<br />

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