The nonlinear heat release response of stratified lean-premixed flames to acoustic velocity oscillations

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This paper analyzes the forced response of swirl-stabilized lean-premixed flames to high-amplitude acoustic forcing in a laboratory-scale stratified burner operated with CH(4) and air at atmospheric pressure. The double-swirler, double-channel annular burner was specially designed to generate high-amplitude acoustic velocity oscillations and a radial equivalence ratio gradient at the inlet of the combustion chamber. Temporal oscillations of equivalence ratio along the axial direction are dissipated over a long distance, and therefore the effects of time-varying fuel/air ratio on the response are not considered in the present investigation. Simultaneous measurements of inlet velocity and heat release rate oscillations were made using a constant temperature anemometer and photomultiplier tubes with narrow-band OH*/CH* interference filters. Time-averaged and phase-synchronized CH* chemiluminescence intensities were measured using an intensified CCD camera. The measurements show that flame stabilization mechanisms vary depending on equivalence ratio gradients for a constant global equivalence ratio (phi(g) = 0.60). Under uniformly premixed conditions, an enveloped M-shaped flame is observed. In contrast, under stratified conditions, a dihedral V-flame and a toroidal detached flame develop in the outer stream and inner stream fuel enrichment cases, respectively. The modification of the stabilization mechanism has a significant impact on the nonlinear response of stratified flames to high-amplitude acoustic forcing (u'/U similar to 0.45 and f = 60, 160 Hz). Outer stream enrichment tends to improve the flame's stiffness with respect to incident acoustic/vortical disturbances, whereas inner stream stratification tends to enhance the nonlinear flame dynamics, as manifested by the complex interaction between the swirl flame and large-scale coherent vortices with different length scales and shedding points. It was found that the behavior of the measured flame describing functions (FDF), which depend on radial fuel stratification, are well correlated with previous measurements of the intensity of self-excited combustion instabilities in the stratified swirl burner. The results presented in this paper provide insight into the impact of non-uniform reactant stoichiometry on combustion instabilities, its effect on flame location and the interaction with unsteady flow structures.
Publisher
ELSEVIER SCIENCE INC
Issue Date
2011-12
Language
English
Article Type
Article
Keywords

SWIRL-STABILIZED COMBUSTOR; TURBINE MODEL COMBUSTOR; KINEMATIC MODEL; DUCTED FLAME; FLOW; DYNAMICS; PROPAGATION; WAVES; DISTURBANCES; DIAGNOSTICS

Citation

COMBUSTION AND FLAME, v.158, no.12, pp.2482 - 2499

ISSN
0010-2180
DOI
10.1016/j.combustflame.2011.05.016
URI
http://hdl.handle.net/10203/207570
Appears in Collection
AE-Journal Papers(저널논문)
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