55th AIAA Aerospace Sciences Meeting 2017
DOI: 10.2514/6.2017-1954
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Lean Blowout and Ignition Characteristics of Conventional and Surrogate Fuels Measured in a Swirl Stabilized Combustor

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Cited by 41 publications
(19 citation statements)
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“…In addition to chemistry and mixing effects, blowoff is also influenced by atomization and vaporization processes. Available data often generate conflicting or inconclusive results [8][9][10][11][12][13][14][15], likely due to the range of potentially dominant physical processes depending upon atomization quality, air preheat temperature, etc. Early approaches to this problem involved generalizing methods developed from premixed combustors.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…In addition to chemistry and mixing effects, blowoff is also influenced by atomization and vaporization processes. Available data often generate conflicting or inconclusive results [8][9][10][11][12][13][14][15], likely due to the range of potentially dominant physical processes depending upon atomization quality, air preheat temperature, etc. Early approaches to this problem involved generalizing methods developed from premixed combustors.…”
Section: Introductionmentioning
confidence: 99%
“…Other studies have noted kinetic sensitivities to LBO boundaries. For example, Colket et al [10], Stouffer et al [14], and Allision et al [17] found that blowoff boundaries could be correlated with the derived cetane number (DCN), a kinetic property. Although the DCN is directly related to the mixture's ignition delay time [18], it is also correlated with high-temperature kinetic properties, such as the flame speed and the extinction stretch rate [19].…”
Section: Introductionmentioning
confidence: 99%
“…[16]. On comparing kerosene fuels, the kerosene flames with a high derived cetane number (DCN) are more stable than those with a low DCN [15,17,18]. The spray characteristics near blow-off of alternative fuels were compared to A2 in Ref.…”
mentioning
confidence: 99%
“…The referee combustor is experimentally characterized in an apparatus (“referee rig”) that includes an air plenum and bypass flow passages that establish flow splits representative of an engine. 27 Air from compressor outlet splits and enters into numerous air passages within and around the combustor. A fraction of the total air flows through inner axial swirler, outer axial swirler, radial swirler, and swirler cooling slot.…”
Section: Computational Methodologymentioning
confidence: 99%