On Burning Rate and Flame Extinction for Toluene Droplets in Low Gravity

Toluene (C6H5CH3, boiling point of 384 K) is a monocyclic aromatic compound found in transportation fuels, which plays an important role in soot formation during combustion. To understand its combustion and sooting dynamics, an attractive experimental platform is the spherically symmetric droplet flame. In this work, droplet combustion experiments carried out on the International Space Station are reported to study near spherically symmetric burning of untethered or free-floating toluene droplets at atmospheric pressure over a wide range of initial droplet diameters (D0 ∼ 1 to 7 mm). Spherically symmetric burning conditions and one-dimensional gas transport provide a useful environment to reveal the burning characteristics of this complex fuel, including the influence of D0 on radiative transport, fuel burning rate, and flame extinction. Results showed that droplets burned to completion without experiencing radiative extinction for D0 < 2.5 mm, while a two-stage burning process was noted for larger droplets: steady combustion with a visible flame, and then radiative extinction, after which the droplets continued to evaporate because of thermal transport from the locally hot ambience. After radiative extinction, wideband and narrowband radiometer measurements indicated no cool flame or low-temperature combustion regimes. Results also showed that the extinction diameter increased with D0, which is consistent with trends previously reported for other hydrocarbon fuels. The instantaneous droplet burning rate (K) was initially steady as combustion developed and then decreased with time, accompanied by a significant reduction in flame radiance when the flame radiatively extinguished. A scaling analysis by an energy balance at the droplet interface revealed that the estimated flame temperature dropped sharply from approximately 1400 to 560 K shortly after radiative extinction and then gradually decreased toward ambient levels. Finally, an averaged K (Kavg) was obtained for each D0 in the visible flame regime and correlated by a power law relation Kavg ∼ D0–n.

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Publication Details

Journal
Energy & Fuels
Published
2026-01-29
DOI
https://doi.org/10.1021/acs.energyfuels.5c05103
Citations
1
Primary Topic
Combustion and flame dynamics
Type
article
Field-Weighted Citation Impact
41.77
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article

On Burning Rate and Flame Extinction for Toluene Droplets in Low Gravity

Yuhao Xu, M. Hicks, Xi Liu, Minghui Xu et al.
1 citations
Energy & Fuels
Combustion and flame dynamics
41.77
article

On Burning Rate and Flame Extinction for Toluene Droplets in Low Gravity

Yuhao Xu, M. Hicks, Xi Liu, Minghui Xu, C. Thomas Avedisian
article en
1 citations

Abstract

Toluene (C6H5CH3, boiling point of 384 K) is a monocyclic aromatic compound found in transportation fuels, which plays an important role in soot formation during combustion. To understand its combustion and sooting dynamics, an attractive experimental platform is the spherically symmetric droplet flame. In this work, droplet combustion experiments carried out on the International Space Station are reported to study near spherically symmetric burning of untethered or free-floating toluene droplets at atmospheric pressure over a wide range of initial droplet diameters (D0 ∼ 1 to 7 mm). Spherically symmetric burning conditions and one-dimensional gas transport provide a useful environment to reveal the burning characteristics of this complex fuel, including the influence of D0 on radiative transport, fuel burning rate, and flame extinction. Results showed that droplets burned to completion without experiencing radiative extinction for D0 < 2.5 mm, while a two-stage burning process was noted for larger droplets: steady combustion with a visible flame, and then radiative extinction, after which the droplets continued to evaporate because of thermal transport from the locally hot ambience. After radiative extinction, wideband and narrowband radiometer measurements indicated no cool flame or low-temperature combustion regimes. Results also showed that the extinction diameter increased with D0, which is consistent with trends previously reported for other hydrocarbon fuels. The instantaneous droplet burning rate (K) was initially steady as combustion developed and then decreased with time, accompanied by a significant reduction in flame radiance when the flame radiatively extinguished. A scaling analysis by an energy balance at the droplet interface revealed that the estimated flame temperature dropped sharply from approximately 1400 to 560 K shortly after radiative extinction and then gradually decreased toward ambient levels. Finally, an averaged K (Kavg) was obtained for each D0 in the visible flame regime and correlated by a power law relation Kavg ∼ D0–n.

Energy & FuelsVol. 40(6)
Cornell University (US), Glenn Research Center (US), Combustion Institute (US), Sibley Memorial Hospital (US), Clemson University (US)
Openalex Percentile: Top 1%
Combustion and flame dynamics
41.77
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