THERMOACOUSTIC INSTABILITIES OF HYDROGEN-ENRICHED PARTIALLY PREMIXED FLAMES IN A SWIRL COMBUSTOR

被引:0
|
作者
Gong, Y. [1 ]
Fredrich, D. [1 ]
Marquis, A. J. [1 ]
Jones, W. P. [1 ]
Boxx, I. [2 ]
机构
[1] Imperial Coll London, Dept Mech Engn, London, England
[2] German Aerosp Ctr DLR, Stuttgart, Germany
基金
欧洲研究理事会; 英国工程与自然科学研究理事会;
关键词
LARGE-EDDY SIMULATION; BOUNDARY-CONDITIONS; IGNITION; METHANE; NO;
D O I
暂无
中图分类号
O414.1 [热力学];
学科分类号
摘要
Large eddy simulations (LES) of premixed hydrogen-enriched swirling flames were performed to investigate the flame topology and combustion instabilities with different hydrogen concentrations. A compressible LES approach is utilised to account for the self-excited combustion dynamics. A transported probability density function (pdf) approach is adopted to account for sub-grid scale (sgs) turbulence-chemistry interaction, and the solution to the joint sgs pd f evolution equation of the scalars is obtained by the stochastic field method. The chemistry is represented using a reduced chemical reaction mechanism containing 15 reaction steps and 19 species. The results revealed that as the concentration of hydrogen increases, the flame is shortened in the injecting direction and more confined in the cross-sectional direction, which is consistent with experimental observations. The self-excited limit-cycle oscillations for all considered cases were successfully reproduced, with the predicted peak frequencies of the chamber pressure spectra in excellent agreement with the measured values. The feedback loop of the oscillations is successfully captured and analysed with the temporal evolution of axial velocity and heat release presented.
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页数:8
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