TY - JOUR
T1 - Radiation of noise in turbulent non-premixed flames
AU - Ihme, Matthias
AU - Pitsch, Heinz
AU - Bodony, Daniel
N1 - Funding Information:
The authors gratefully acknowledge funding by the United States Department of Energy within the Advanced Simulation and Computing (ASC) program. Helpful discussions with Sanjiva Lele are gratefully acknowledged. We thank Andreas Dreizler, Jay P. Gore, and Kapil K. Singh for sharing their experimental data with us.
PY - 2009
Y1 - 2009
N2 - A model for the prediction of combustion-generated noise in non-premixed flames has been developed. This model is based on Lighthill's acoustic analogy and employs the flamelet/progress variable model to express the excess density as function of mixture fraction and reaction progress variable. In this model, three major sources of sound have been identified, and their individual contribution to the acoustic spectra and overall sound pressure level are analyzed for a nitrogen-diluted methane-hydrogen/air flame. The hybrid approach, combining a large-eddy simulation and a computational aeroacoustic method, introduces spurious noise which can pollute the acoustic results. All relevant sources of spurious noise are analyzed, and a physics-based low-pass filter is proposed which eliminates spurious noise due to the convection of acoustic sources. The numerical predictions for both statistical flow field quantities and acoustic results have been validated with experimental data. The good agreement between experiments and simulation highlights the potential of the method for applications to more complex flow configurations and to provide further understanding of combustion noise mechanisms.
AB - A model for the prediction of combustion-generated noise in non-premixed flames has been developed. This model is based on Lighthill's acoustic analogy and employs the flamelet/progress variable model to express the excess density as function of mixture fraction and reaction progress variable. In this model, three major sources of sound have been identified, and their individual contribution to the acoustic spectra and overall sound pressure level are analyzed for a nitrogen-diluted methane-hydrogen/air flame. The hybrid approach, combining a large-eddy simulation and a computational aeroacoustic method, introduces spurious noise which can pollute the acoustic results. All relevant sources of spurious noise are analyzed, and a physics-based low-pass filter is proposed which eliminates spurious noise due to the convection of acoustic sources. The numerical predictions for both statistical flow field quantities and acoustic results have been validated with experimental data. The good agreement between experiments and simulation highlights the potential of the method for applications to more complex flow configurations and to provide further understanding of combustion noise mechanisms.
KW - Aeroacoustics
KW - Combustion-noise
KW - Computational aeroacoustics
KW - Large-eddy simulation
KW - Turbulent non-premixed combustion
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U2 - 10.1016/j.proci.2008.06.137
DO - 10.1016/j.proci.2008.06.137
M3 - Conference article
AN - SCOPUS:67649259154
SN - 1540-7489
VL - 32 I
SP - 1545
EP - 1553
JO - Proceedings of the Combustion Institute
JF - Proceedings of the Combustion Institute
IS - 1
T2 - 32nd International Symposium on Combustion
Y2 - 3 August 2008 through 8 August 2008
ER -