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Mixing in a model gas turbine combustor studied by panoramic optical techniques

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Thermophysics and Aeromechanics Aims and scope

Abstract

Using planar optical methods based on laser-induced fluorescence and particle image velocimetry instantaneous velocity fields and passive tracer concentration are measured simultaneously in a model of GT-combustor at realistic flow rates. Spatial distributions of velocity pulsations and passive tracer concentration pulsations are measured at air flow rate about 0.4 kg/s. Correlations of velocity and concentration pulsations are measured. The most intense turbulent mass flux in the region of swirling flow mixing layer was observed. The contribution of advective and turbulent components in the transfer of a passive tracer in the axial direction was estimated.

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Correspondence to L. M. Chikishev.

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This work was financially supported by the Russian Science Foundation (Grant No. 14-29-00203).

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Chikishev, L.M., Dulin, V.M., Gobyzov, O.A. et al. Mixing in a model gas turbine combustor studied by panoramic optical techniques. Thermophys. Aeromech. 24, 347–353 (2017). https://doi.org/10.1134/S0869864317030039

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  • DOI: https://doi.org/10.1134/S0869864317030039

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