4.3 Article

Correspondence Between Stable Flame Macrostructure and Thermo-Acoustic Instability in Premixed Swirl-Stabilized Turbulent Combustion

Publisher

ASME
DOI: 10.1115/1.4029173

Keywords

-

Funding

  1. King Fahd University of Petroleum and Minerals (KFUPM)
  2. Abdullah University of Science and Technology (KAUST) in Saudi Arabia [R12-CE-10, KUS-110-010-01]

Ask authors/readers for more resources

In this paper, we conduct an experimental investigation to study the link between the flame macroscale structure-or flame brush spatial distribution-and thermo-acoustic instabilities, in a premixed swirl-stabilized dump combustor. We operate the combustor with premixed methane-air in the range of equivalence ratio (phi) from the lean blowout limit to phi = 0: 75. First, we observe the different dynamic modes in this lean range as phi is raised. We also document the effect of phi on the flame macrostructure. Next, we examine the correspondence between dynamic mode transitions and changes in flame macrostructure. To do so, we modify the combustor length-by downstream truncation-without changing the underlying flow upstream. Thus, the resonant frequencies of the geometry are altered allowing for decoupling the heat release rate fluctuations and the acoustic feedback. Mean flame configurations in the modified combustor and for the same range of equivalence ratio are examined, following the same experimental protocol. It is found that not only the same sequence of flame macrostructures is observed in both combustors but also that the transitions occur at a similar set of equivalence ratio. In particular, the appearance of the flame in the outside recirculation zone (ORZ) in the long combustor-which occurs simultaneously with the onset of instability at the fundamental frequency-happens at similar phi when compared to the short combustor, but without being in latter case accompanied by a transition to thermo-acoustic instability. Then, we interrogate the flow field by analyzing the streamlines, mean, and rms velocities for the nonreacting flow and the different flame types. Finally, we focus on the transition of the flame to the ORZ in the acoustically decoupled case. Our analysis of this transition shows that it occurs gradually with an intermittent appearance of a flame in the ORZ and an increasing probability with phi. The spectral analysis of this phenomenon-we refer to as ORZ flame flickering-shows the presence of unsteady events occurring at two distinct low frequency ranges. A broad band at very low frequency in the range similar to(1 Hz-10 Hz) associated with the expansion and contraction of the inner recirculation zone (IRZ) and a narrow band centered around 28 Hz which is the frequency of rotation of the flame as it is advected by the ORZ flow.

Authors

I am an author on this paper
Click your name to claim this paper and add it to your profile.

Reviews

Primary Rating

4.3
Not enough ratings

Secondary Ratings

Novelty
-
Significance
-
Scientific rigor
-
Rate this paper

Recommended

No Data Available
No Data Available