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Accounting for convective effects in zero-Mach-number thermoacoustic models

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Academic year: 2021

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Figure

Fig. 1. Schematic view of the proposed modelling strategy. (a) The whole domain is computed while taking the mean flow into account and (b) the combustion chamber is solved under the zero Mach number assumption
Fig. 2. Schematic representation of the boundary between a domain computed with a Helmholtz solver and a finite Mach number acoustic element.
Table 3 summarises the analytical procedures described above.
Fig. 4. Frequency (a) and growth rate (b) of the first eigenmode for different inlet Mach number M 1 for the computation of the global domain (
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