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Second Computational Aeroacoustics (CAA) Workshop on ...

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I. ANALYTICAL SOLUTION OF THE PROBLEM 2<br />

This is an initial-value problem governedby the linearized Euler equati<strong>on</strong>s<br />

The initial c<strong>on</strong>diti<strong>on</strong>s are:<br />

and<br />

Here xs = 4, w = 0.2.<br />

and<br />

by<br />

The boundary c<strong>on</strong>diti<strong>on</strong>s are:<br />

Ou Op<br />

-_ + N = 0 (28)<br />

Ov Op<br />

N + _yy = 0 (29)<br />

Op Ou Ov<br />

N + _ + N = 0 (30)<br />

u=v=0 at t 0 (31)<br />

p(x, y, 0) = e -u'2((,-*'):+y2)/w2<br />

l<br />

at t = 0 (32) _*<br />

v.n=O at x 2+y2=(0.5) 2, (33)<br />

when x, y ---+ oc the soluti<strong>on</strong> respresents outgoing waves. (34)<br />

Soluti<strong>on</strong> of the problem (28) - (34) can be found in terms of velocity potential ¢(x, y, t) defined<br />

0¢ 0¢ 0¢<br />

= N' "= 0_' p - ot (35)<br />

It is easy to show from (28) - (30) and (35) that the governing equati<strong>on</strong> for ¢ is the wave equa-<br />

ti<strong>on</strong> which may be written in polar coordinates (r, O) as<br />

Initial c<strong>on</strong>diti<strong>on</strong>s (31) and (32) are reduced to<br />

t=O:<br />

1<br />

02¢ f82¢ 10¢ __02¢_<br />

Ot 2 \ Or 2 + r -_r + r 2 002 ,] = 0 (36)<br />

¢=0, Ot - e (37)<br />

12<br />

=<br />

i<br />

Ii<br />

E<br />

l<br />

E<br />

E

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