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Numerical Simulation of the Dynamics of Turbulent Swirling Flames

Numerical Simulation of the Dynamics of Turbulent Swirling Flames

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Response <strong>of</strong> Premixed <strong>Flames</strong> to Velocity Disturbances<br />

surements at <strong>the</strong> burner exit at two different frequencies to identify <strong>the</strong> varied<br />

propagations speeds <strong>of</strong> <strong>the</strong> perturbations and <strong>the</strong> variations <strong>of</strong> swirl number<br />

produced by <strong>the</strong>m. The impact <strong>of</strong> <strong>the</strong> variations <strong>of</strong> swirl number and by <strong>the</strong><br />

phase between perturbations on <strong>the</strong> flame response was analyzed. It was observed<br />

that when <strong>the</strong> axial and tangential velocity fluctuations were almost<br />

out <strong>of</strong> phase, swirl number fluctuations were present, inducing variations on<br />

<strong>the</strong> flame angle. Under <strong>the</strong>se conditions, a destructive interaction mechanism<br />

is produced, which decreases <strong>the</strong> amplitude <strong>of</strong> <strong>the</strong> flame describing function.<br />

On <strong>the</strong> o<strong>the</strong>r hand, when both perturbations were almost in phase, <strong>the</strong> amplitude<br />

<strong>of</strong> <strong>the</strong> swirl number fluctuation decreased, and a constructive interaction<br />

mechanism is produced, showing a peak amplitude in <strong>the</strong> flame describing<br />

function. The investigations mentioned before demonstrate that <strong>the</strong> position<br />

<strong>of</strong> <strong>the</strong> swirler has a strong impact on <strong>the</strong> flame response.<br />

Finally, non-linearity is also an important issue on <strong>the</strong> studies <strong>of</strong> flame dynamics.<br />

It appears from a saturation response <strong>of</strong> <strong>the</strong> flame to <strong>the</strong> increase <strong>of</strong><br />

<strong>the</strong> amplitude <strong>of</strong> <strong>the</strong> fluctuation. This topic is not investigated in <strong>the</strong> present<br />

study as it is focus on <strong>the</strong> use <strong>of</strong> tools in <strong>the</strong> linear regime as linear system<br />

identification with finite impulse response filters and network models using<br />

linearized Navier-Stokes equations. Thus <strong>the</strong> flame was excited to amplitudes<br />

in <strong>the</strong> linear regime <strong>of</strong> <strong>the</strong> flame [96]. While experimental and analytical investigations<br />

has been extensively carried out in <strong>the</strong> investigation <strong>of</strong> non-linear<br />

effects, <strong>the</strong> development <strong>of</strong> non-linear system identification tools for <strong>the</strong>rmoacoustics<br />

systems [157, 182, 183] is in its early stages, showing that a much<br />

complex process needs to be carried out for <strong>the</strong> identification compared to<br />

<strong>the</strong> linear identification tools.<br />

3.4 Model <strong>of</strong> Impulse and Frequency Responses to Axial Velocity<br />

and Swirl Fluctuations<br />

Various models have been proposed to describe <strong>the</strong> flame response as mentioned<br />

in section 3.2. Some <strong>of</strong> <strong>the</strong>se models are based on time lag distributions.<br />

A model for <strong>the</strong> flame dynamics was proposed by Komarek and Po-<br />

48

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