THESE de DOCTORAT - cerfacs
THESE de DOCTORAT - cerfacs
THESE de DOCTORAT - cerfacs
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1.2 Scope of the present work 17<br />
flame and consequently influencing it by modifying the heat release. When an unstable<br />
coupling of this nature takes place, one will talk about ‘thermoacoustics instabilities’<br />
[78, 22]. This is a broad field of study within the combustion community [48]. Efforts<br />
have been done over several <strong>de</strong>ca<strong>de</strong>s to un<strong>de</strong>rstand the influence of acoustics on flame<br />
dynamics [78, 18, 19, 73, 87, 49, 86, 88, 63]<br />
Un<strong>de</strong>rstanding combustion noise in real engines means un<strong>de</strong>rstanding all these coupled phenomena.<br />
However, the most clear starting point to study combustion noise is to ‘un-couple’ all<br />
these mechanisms, focusing on one at a time. As a consequence, it is assumed that the sources<br />
of noise (flame, turbulence, etc) are in<strong>de</strong>pen<strong>de</strong>nt of the acoustic field generated. In other words,<br />
that no instabilities occur. Still, the following noise generation phenomena remain and must be<br />
consi<strong>de</strong>red:<br />
• flame/entropy/acoustics → ‘indirect combustion noise’. The sources of noise are the<br />
entropy waves when crossing non-homogeneous regions (zones with mean flow gradients).<br />
• Turbulence/acoustics → ‘aerodynamic noise’. The unsteady turbulent field is the source<br />
of noise. The influence of walls as scattering/reflecting mechanism (ex: wing airfoils, cavities)<br />
are also usually consi<strong>de</strong>red into the physical formulations.<br />
• flame/acoustics → ‘direct combustion noise’. The unsteady heat release acts as a distribution<br />
of acoustic monopoles, which generate pressure fluctuations.<br />
1.2 Scope of the present work<br />
Combustion noise has been wi<strong>de</strong>ly studied in open flames. These predictions are based on<br />
what is known as hybrid methods. In these approaches the sources of noise are computed separately<br />
from the radiated acoustic field. Unsteady CFD methods such as LES or DNS are used<br />
to compute the sources of noise whereas wave equations coming from acoustic analogies are<br />
employed to compute the sound radiation produced by these sources. LES or DNS are rarely<br />
used to estimate acoustic fluctuations directly, since these fluctuations are much smaller in<br />
comparison to first or<strong>de</strong>r fluctuations, as velocity or temperature perturbations. The first objective<br />
of this thesis regards this concern. It is seen how much the computation resolution of LES<br />
influences the quality of the estimations of noise. A second objective is linked to the hybrid approach<br />
for the estimation of combustion noise. No significative studies within the combustion<br />
community have been performed to evaluate whether or not hybrid approaches are appropriate<br />
to compute noise of confined flames. Confinement of flames leads to possible complexities:<br />
one of them is that pressure fluctuations produced by the flame might contain an important<br />
contribution of hydrodynamics, since in confined flames turbulence might be significant everywhere.<br />
Another significant concern is the evaluation of acoustic-flow interactions. When