22.10.2014 Views

THESE de DOCTORAT - cerfacs

THESE de DOCTORAT - cerfacs

THESE de DOCTORAT - cerfacs

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

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

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!