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THESE de DOCTORAT - cerfacs

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86 Chapter 5: Assessment of combustion noise in a premixed swirled combustor<br />

Pressure Fluctuation (Pa)<br />

M5 M6 M7<br />

40<br />

Premixer<br />

Combustion chamber<br />

20<br />

0<br />

−20<br />

−40<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 />

40<br />

Premixer<br />

Combustion chamber<br />

20<br />

0<br />

−20<br />

−40<br />

−0.2 −0.1 0 0.1 0.2<br />

x (m)<br />

0.3 0.4 0.5<br />

(b) Pressure fluctuation from LES<br />

Direct Computation<br />

Figure 5.17: Longitudinal pressure Waves oscillating at 954 Hz<br />

Pressure Fluctuation (Pa)<br />

M5 M6 M7<br />

40<br />

Premixer<br />

Combustion chamber<br />

20<br />

0<br />

−20<br />

−40<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 />

40<br />

Premixer<br />

Combustion chamber<br />

20<br />

0<br />

−20<br />

−40<br />

−0.2 −0.1 0 0.1 0.2<br />

x (m)<br />

0.3 0.4 0.5<br />

(b) Pressure fluctuation from LES<br />

Direct Computation<br />

Figure 5.18: Longitudinal pressure Waves oscillating at 1658 Hz

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