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THESE de DOCTORAT - cerfacs

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6.6 Transmitted and Reflected Waves through an i<strong>de</strong>al Compressor: the enthalpy jump case 117<br />

ˆp t<br />

ˆp t,1<br />

=<br />

¯p t<br />

¯p t,1<br />

thus<br />

∂ ˆp t<br />

∂x = ˆp t,1 ∂ ¯p t<br />

¯p t,1 ∂x<br />

(6.64)<br />

The profile of ˆp t is given by a smooth hyperbolic tangent relation as seen in Fig. 6.14. From<br />

Eq. (6.64), the (∂ ˆp t /∂x) term in Eq. (6.63) must be written as<br />

x m<br />

x ups<br />

2<br />

¯p t / ¯p t1<br />

| ˆp t |/|ˆp t1 |<br />

1.8<br />

1.6<br />

1.4<br />

1.2<br />

1<br />

0 0.1 0.2 0.3 0.4<br />

X (m)<br />

Figure 6.14: Mean and Fluctuation profiles of total pressure<br />

∂ ˆp t<br />

∂x = ˆp t1 f (x, ¯π c ) with (6.65)<br />

[ ( )] [ ]<br />

f (x, π c ) = 0.5 ( ¯π c − 1) 1 − tanh 2 k(x − xm ) k<br />

(6.66)<br />

x m − x ups x m − x ups<br />

6.6.4 Results<br />

Two different cases are consi<strong>de</strong>red, corresponding to two different values of π c = ¯p t2 / ¯p t1 . The<br />

value of the reflection coefficient R = w + 2 /w− 2<br />

is computed by using both the analytical and the<br />

numerical approach (SNozzle). In or<strong>de</strong>r to observe the influence of the forcing frequency on<br />

the values of R, results are plotted as a function of a non-dimensional frequency.<br />

Ω = f L/ ¯c 2 (6.67)<br />

where L represents the length of the compressor and ¯c 2 the velocity of sound at the outlet. The

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