THESE de DOCTORAT - cerfacs
THESE de DOCTORAT - cerfacs
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