TY - JOUR
T1 - Measurement of flame transfer functions in swirl-stabilized, lean-premixed combustion
AU - Ranalli, J. A.
AU - Martin, C. R.
AU - Black, P. R.
AU - Vandsburger, U.
AU - West, R.
N1 - Funding Information:
The authors acknowledge the financial support of the Department of Energy through the University Turbine Research Program and the South Carolina Institute of Energy Studies. Author J. Ranalli would also like to thank the U.S. Department of Defense for funding through the National Defense Science and Engineering Graduate Fellowship.
PY - 2009
Y1 - 2009
N2 - Results of ongoing experimental measurements of lean-premixed combustion flame dynamics, necessary to further predictive capabilities of models for combustion instabilities, was studied. Two possible mechanisms were considered for the study, including coupling through velocity and equivalence ratio oscillations. Experiments were carried out on a rig specifically designed for gaseous, premixed, turbulent combustion experiments. Swirl was generated by a fixed-vane swirler with vanes at a 30 deg angle to the flow axis. Fuel flows were specified to provide mean equivalence ratios for both natural gas and propane. The flame output was measured relative to each of these perturbations, resulting in the FTF. Low-frequency gain exhibited an increasing trend with respect to mean equivalence ratio for the case of velocity perturbations, but remained practically constant for the case of equivalence ratio perturbations. Time delay was slightly shorter for equivalence ratio perturbations, however, no significant variation in the delay is observed between fuels.
AB - Results of ongoing experimental measurements of lean-premixed combustion flame dynamics, necessary to further predictive capabilities of models for combustion instabilities, was studied. Two possible mechanisms were considered for the study, including coupling through velocity and equivalence ratio oscillations. Experiments were carried out on a rig specifically designed for gaseous, premixed, turbulent combustion experiments. Swirl was generated by a fixed-vane swirler with vanes at a 30 deg angle to the flow axis. Fuel flows were specified to provide mean equivalence ratios for both natural gas and propane. The flame output was measured relative to each of these perturbations, resulting in the FTF. Low-frequency gain exhibited an increasing trend with respect to mean equivalence ratio for the case of velocity perturbations, but remained practically constant for the case of equivalence ratio perturbations. Time delay was slightly shorter for equivalence ratio perturbations, however, no significant variation in the delay is observed between fuels.
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U2 - 10.2514/1.44187
DO - 10.2514/1.44187
M3 - Article
AN - SCOPUS:72949103052
SN - 0748-4658
VL - 25
SP - 1350
EP - 1354
JO - Journal of Propulsion and Power
JF - Journal of Propulsion and Power
IS - 6
ER -