THESE de DOCTORAT - cerfacs
THESE de DOCTORAT - cerfacs
THESE de DOCTORAT - cerfacs
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5.3 Combustion noise Analysis 85<br />
Pressure Fluctuation (Pa)<br />
M5 M6 M7<br />
1000<br />
Premixer<br />
Combustion chamber<br />
500<br />
0<br />
−500<br />
−1000<br />
−0.2 −0.1 0 0.1 0.2<br />
x (m)<br />
0.3 0.4 0.5<br />
(a) Quarter pressure Wave from Eq. (2.63)<br />
Hybrid Computation<br />
Pressure Fluctuation (Pa)<br />
M5 M6 M7<br />
1000<br />
Premixer<br />
Combustion chamber<br />
500<br />
0<br />
−500<br />
−1000<br />
−0.2 −0.1 0 0.1 0.2<br />
x (m)<br />
0.3 0.4 0.5<br />
(b) Quarter pressure Wave from LES<br />
Direct Computation<br />
Figure 5.15: Longitudinal pressure waves oscillating at 377 Hz<br />
cillation to be triggered in this region.<br />
Pressure Fluctuation (Pa)<br />
M5 M6 M7<br />
600<br />
Premixer<br />
Combustion chamber<br />
400<br />
200<br />
0<br />
−200<br />
−400<br />
−600<br />
−0.2 −0.1 0 0.1 0.2<br />
x (m)<br />
0.3 0.4 0.5<br />
(a) Pressure Wave from Eq. (2.63)<br />
Hybrid Computation<br />
Pressure Fluctuation (Pa)<br />
M5 M6 M7<br />
600<br />
Premixer<br />
Combustion chamber<br />
400<br />
200<br />
0<br />
−200<br />
−400<br />
−600<br />
−0.2 −0.1 0 0.1 0.2<br />
x (m)<br />
0.3 0.4 0.5<br />
(b) Pressure Wave from LES<br />
Direct Computation<br />
Figure 5.16: Longitudinal pressure waves oscillating at 251 Hz<br />
In Fig. 5.17 two different types of pressure waves are observed at microphone 5 for the direct<br />
and hybrid computations in the region around 1000 Hz. Whereas a pure acoustic standing<br />
wave is obtained by the hybrid approach, a perturbed pressure wave is obtained in the direct<br />
computation results. A pure standing acoustic wave can naturally have an acoustic pressure<br />
no<strong>de</strong>. If this pressure no<strong>de</strong> is present close to the region of the measurement <strong>de</strong>vice a low<br />
value of pressure fluctuation will be obtained. This is what happens for microphone 5 in the<br />
zone close to 1000 Hz (Fig. 5.17a). Obviously, when the pressure fluctuations not only contain<br />
acoustics but also hydrodynamic perturbations as in the direct computations (Fig. 5.17b),<br />
no pressure no<strong>de</strong> can be observed and the resulting SPL is much higher than in the hybrid<br />
computation case. Similar conclusions can be drawn at frequencies around 1650 Hz where a<br />
pressure no<strong>de</strong> is found close to Microphone 6 (Fig. 5.18).<br />
In or<strong>de</strong>r to not have any ambiguity measuring acoustic pressure fluctuations due to the presence<br />
of pressure no<strong>de</strong>s, a more appropriate quantity to evaluate at the microphone positions is