Evaluation of thermoacoustic instability for chemically reacting flows using large-eddy simulations
Thermoacoustic instability for chemically reacting flows was investigated using large eddy simulations coupled with a lookup table for turbulence-chemistry closure. The onset of instability was evaluated from pressure fluctuations, as well as standard and extended Rayleigh criterion, as suggested in...
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sg-ntu-dr.10356-1746912024-04-13T16:48:57Z Evaluation of thermoacoustic instability for chemically reacting flows using large-eddy simulations Lim, Wei Xian Chan, Wai Lee Elhadidi, Basman School of Mechanical and Aerospace Engineering Engineering Combustors Large eddy simulation Thermoacoustic instability for chemically reacting flows was investigated using large eddy simulations coupled with a lookup table for turbulence-chemistry closure. The onset of instability was evaluated from pressure fluctuations, as well as standard and extended Rayleigh criterion, as suggested in literature. Two configurations were considered, namely, a canonical Rijke tube and a simplified can combustor with a swirling flow injector representing a complex generalized geometry. For the Rijke tube, premixed and nonpremixed combustion models were applied for identical fuel flowrate, resulting in different thermoacoustic outcomes due to differences in reaction rates of the two flame regimes. Results from the Rijke tube case agree with analytic thermoacoustic theory. For the can combustor, only premixed chemistry was considered as it better represents the experimental conditions, and the first resonant pressure mode aligns reasonably with published experimental data. Findings suggest that, if thermoacoustic instability is detected, the resonant frequency can be deduced from the fluctuations of the pressure, heat release, or acoustic source term. However, even though the resonant frequency is correctly identified, fluctuation data alone is insufficient to identify the onset of thermoacoustic instability, requiring the additional application of Rayleigh criterion. Finally, this study concludes that, for the range of configurations evaluated here, the standard Rayleigh criterion is sufficient to determine the onset of thermoacoustic instability, so the extended Rayleigh criterion is not always necessary, in contrast to suggestions from previous work. This conclusion is significant because the standard Rayleigh criterion is the only practical evaluation for physical experiments. Submitted/Accepted version 2024-04-08T01:42:56Z 2024-04-08T01:42:56Z 2024 Journal Article Lim, W. X., Chan, W. L. & Elhadidi, B. (2024). Evaluation of thermoacoustic instability for chemically reacting flows using large-eddy simulations. Journal of Fluids Engineering, 146(6), 061203-. https://dx.doi.org/10.1115/1.4064385 0098-2202 https://hdl.handle.net/10356/174691 10.1115/1.4064385 2-s2.0-85185397917 6 146 061203 en Journal of Fluids Engineering © 2024 ASME. All rights reserved. This article may be downloaded for personal use only. Any other use requires prior permission of the copyright holder. The Version of Record is available online at http://doi.org/10.1115/1.4064385. application/pdf |
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Engineering Combustors Large eddy simulation Lim, Wei Xian Chan, Wai Lee Elhadidi, Basman Evaluation of thermoacoustic instability for chemically reacting flows using large-eddy simulations |
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Thermoacoustic instability for chemically reacting flows was investigated using large eddy simulations coupled with a lookup table for turbulence-chemistry closure. The onset of instability was evaluated from pressure fluctuations, as well as standard and extended Rayleigh criterion, as suggested in literature. Two configurations were considered, namely, a canonical Rijke tube and a simplified can combustor with a swirling flow injector representing a complex generalized geometry. For the Rijke tube, premixed and nonpremixed combustion models were applied for identical fuel flowrate, resulting in different thermoacoustic outcomes due to differences in reaction rates of the two flame regimes. Results from the Rijke tube case agree with analytic thermoacoustic theory. For the can combustor, only premixed chemistry was considered as it better represents the experimental conditions, and the first resonant pressure mode aligns reasonably with published experimental data. Findings suggest that, if thermoacoustic instability is detected, the resonant frequency can be deduced from the fluctuations of the pressure, heat release, or acoustic source term. However, even though the resonant frequency is correctly identified, fluctuation data alone is insufficient to identify the onset of thermoacoustic instability, requiring the additional application of Rayleigh criterion. Finally, this study concludes that, for the range of configurations evaluated here, the standard Rayleigh criterion is sufficient to determine the onset of thermoacoustic instability, so the extended Rayleigh criterion is not always necessary, in contrast to suggestions from previous work. This conclusion is significant because the standard Rayleigh criterion is the only practical evaluation for physical experiments. |
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School of Mechanical and Aerospace Engineering |
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School of Mechanical and Aerospace Engineering Lim, Wei Xian Chan, Wai Lee Elhadidi, Basman |
format |
Article |
author |
Lim, Wei Xian Chan, Wai Lee Elhadidi, Basman |
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Lim, Wei Xian |
title |
Evaluation of thermoacoustic instability for chemically reacting flows using large-eddy simulations |
title_short |
Evaluation of thermoacoustic instability for chemically reacting flows using large-eddy simulations |
title_full |
Evaluation of thermoacoustic instability for chemically reacting flows using large-eddy simulations |
title_fullStr |
Evaluation of thermoacoustic instability for chemically reacting flows using large-eddy simulations |
title_full_unstemmed |
Evaluation of thermoacoustic instability for chemically reacting flows using large-eddy simulations |
title_sort |
evaluation of thermoacoustic instability for chemically reacting flows using large-eddy simulations |
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2024 |
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https://hdl.handle.net/10356/174691 |
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1800916338055577600 |