2019
DOI: 10.1016/j.supflu.2018.12.010
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Hydrothermal ethanol flames in Co-flow jets

Abstract: Results on the autoignition and stabilization of ethanol hydrothermal fames in a Supercritical Water Oxidation (SCWO) reactor operating at constant pressure are reported. The flames are observed as luminous reaction zones occurring in supercritical water; i.e., water at conditions above its critical point (approximately 22 MPa and 374 °C). A co-flow injector is used to inject fuel (inner flow), comprising an aqueous solution ranging from 20 %-v to 50 %-v ethanol, and air (annular flow) into a reactor filled wi… Show more

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Cited by 36 publications
(19 citation statements)
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References 15 publications
(18 reference statements)
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“…The results showed that the speed increased with injection temperature. In comparison with a higher flame propagation velocity (0.4-3 m/s) in gas phase combustion, the hydrothermal flame propagation velocity varied from 0.01 to 0.1 m/s in the volumetric reactor, which was also consistent with the experimental results by M.C.Hicks [59]. However, it should be noted that due to the fact that the properties of the mixture in the supercritical state cannot be calculated accurately, there is still a deviation for the calculated value.…”
Section: Flame Propagation Speedsupporting
confidence: 89%
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“…The results showed that the speed increased with injection temperature. In comparison with a higher flame propagation velocity (0.4-3 m/s) in gas phase combustion, the hydrothermal flame propagation velocity varied from 0.01 to 0.1 m/s in the volumetric reactor, which was also consistent with the experimental results by M.C.Hicks [59]. However, it should be noted that due to the fact that the properties of the mixture in the supercritical state cannot be calculated accurately, there is still a deviation for the calculated value.…”
Section: Flame Propagation Speedsupporting
confidence: 89%
“…Ignition was the fourth stage in the whole process. Hicks observed the spontaneous ignition of the ethanol-water-air system injected by laminar flow had three stages: random spots, flash-back, and stabilization (see Figure 7) [59]. The results showed that the formation and disappearance of random hot spots might occur more than once before the stable flame was finally established.…”
Section: Ignition Processmentioning
confidence: 96%
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