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Lewis number effect in lean premixed -air and -air flames during thermoacoustic instability in a low-swirl combustor
Phys. Rev. Fluids 10, 043201 – Published 21 April, 2025
DOI: https://doi.org/10.1103/PhysRevFluids.10.043201
Abstract
Suppression of and emissions in gas turbines is an urgent challenge. While lean premixed combustion is a strategy for reducing production, the occurrence of thermoacoustic instability is a significant issue. In addition, while hydrogen is a promising fuel for replacing conventional hydrocarbon fuels and reducing emissions, the unsteady flame-flow dynamics of hydrogen flames under thermoacoustic instabilities remain to be elucidated. Recently, low-swirl combustors have attracted attention since they can stabilize flames with a wide range of fuel compositions including pure hydrogen-air flames. In particular, the characteristics of hydrogen flames are expected to be significantly influenced by its Lewis number Le, where it is for hydrogen-air flames in contrast to for methane-air flames. Therefore, this study experimentally analyzes the Lewis number effect in hydrogen and methane flames during thermoacoustic instability and discuss its influence on the local flame-flow interaction. The flames were stabilized in a low-swirl combustor with a geometric swirl number of 0.39. Pressure fluctuation measurements, OH* chemiluminescence imaging, and particle imaging velocimetry were performed simultaneously. It was found that the pressure fluctuation amplitude was nearly three times larger in the hydrogen flame than in the methane flame. To discuss the Lewis number effect, the instantaneous flame stretch rate and the chemiluminescence intensity were calculated at the local flame tip along the center axis. This analysis revealed that in the hydrogen flame (), the flame stretch rate fluctuation strongly correlated with the chemiluminescence intensity fluctuation, while the correlation between those in the methane flame () was found to be weaker. Therefore, it was concluded that, in the hydrogen flame, the Lewis number effect is responsible for the coupling between the heat release rate fluctuation and the flow fluctuation at the local flame tip during thermoacoustic instability.
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