Abstract

A turbulent flame in an ethanol droplet-laden uniform mixture is investigated at overall equivalence ratios (ϕov) of 0.62, 0.72 and 0.82, using a piloted Bunsen burner. Imaging of OH* chemiluminescence and simultaneous imaging of OH PLIF and Mie scattering, both at 5 kHz, and imaging of CH2O-fuel PLIF at 5 Hz, were used to obtain instantaneous and time-averaged images, temporal sequences and 2-D estimates of flame surface density and curvature. 1-D PDA and LDA measurements were used to obtain droplet size and velocity statistics. At ϕov = 0.62, the flame takes a cylindrical shape, and changes to a cone shape with increasing fuel loading to obtain higher ϕov. Larger droplets are generally observed to have lower average and RMS axial velocities than smaller droplets. Profiles of droplet size distributions indicate a decreasing droplet number density downstream together with a shift to larger droplet diameters. The flame structure is observed to be relatively smooth at locations near the burner exit, and becomes more contorted with distance downstream. In general, droplets are observed to coincide with low-to-intermediate regions of OH. Occasionally, droplets appear to penetrate the flame front, and are detected in regions of intermediate-to-high OH. This occurs particularly at the downstream locations where the flame closes across the jet, with no significant averaged droplet penetration observed past 2 mm in the direction normal to the flame front. Measurements show a gradual reduction in flame surface density and higher flame front curvature with both distance downstream and increasing fuel loading. Estimates of the average droplet evaporation rate increase with both distance downstream and ϕov, as droplets appear in higher mean progress variable regions. The measurements reported here are useful for model validation of flame propagation in dilute sprays.

Highlights

  • Flame propagati on in droplet-laden mixtures is of importance to a variety of practical applications, such as direct-injection IC engines and in gas turbines

  • These trends agreed with estimates of the average droplet vaporization rate, which increased with distance downstream and higher φov

  • The instantaneous flame structure is relatively smooth near the burner exit, with small scale wrinkling developing with distance downstream

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Summary

Introduction

Flame propagati on in droplet-laden mixtures is of importance to a variety of practical applications, such as direct-injection IC engines and in gas turbines. A better understanding of flames in multi-phase flows is crucial to the development of more efficient combustion-based technologies, and the topic continues to be of interest. Detailed experimental measurements are required to validate advanced numerical models to facilitate the development of new technologies. Lent flame propagating in, or stabilised against an incoming flow of, a uniform dispersion of fuel droplets. Similar observations of the effect of droplet size on flame propagation were reported in [5], where the rugged and thickened flame structure observed for large droplet size conditions was suggested to result from incomplete droplet evaporation in the preheat zone, with droplet evaporation continuing into the hot products region of the flame. The resulting increase in the effective volume of the thickened flame structure was suggested to promote combustion and lead to the higher burning velocities measured

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