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Yoo, Chun Sang
Combustion and Propulsion Lab.
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dc.citation.endPage 2056 -
dc.citation.number 2 -
dc.citation.startPage 2049 -
dc.citation.title PROCEEDINGS OF THE COMBUSTION INSTITUTE -
dc.citation.volume 38 -
dc.contributor.author Oh, Suhyeon -
dc.contributor.author Van, Kyu Ho -
dc.contributor.author Jung, Ki Sung -
dc.contributor.author Yoo, Chun Sang -
dc.contributor.author Cha, Min Suk -
dc.contributor.author Chung, Suk Ho -
dc.contributor.author Park, Jeong -
dc.date.accessioned 2023-12-21T16:08:29Z -
dc.date.available 2023-12-21T16:08:29Z -
dc.date.created 2020-09-09 -
dc.date.issued 2021-04 -
dc.description.abstract This study investigates the characteristics of oscillating lifted flames in laminar coflow-jets experimentally and numerically by varying both fuel density (by varying propane and n -butane mixtures) and coflow density (by diluting air with N 2 /He mixtures). Two different lifted flame oscillation behaviors are observed depending on these parameters: oscillating tribrachial lifted flame (OTLF) and oscillating mode-change lifted flame (OMLF), where a rapid increase in flame radius is observed. The regimes of the two flames are identified from experiments, which shows that OMLF occurs only when the effect of the negative buoyancy on the flow field by the fuel heavier than air becomes significant at low fuel jet velocity. OMLFs are also identified to distinguish OTLF regime from flame extinction, which implies that an OMLF can be extinguished when the positive buoyancy becomes weak, losing its stabilizing effect, or when the negative buoyancy becomes strong, further enhancing its destabilizing effect. Transient numerical simulations of both OTLF and OMLF reveal that the OMLF occurs by a strong toroidal vortex and a subsequent counterflow-like structure induced by relatively-strong negative buoyancy. Such a drastic flow redirection significantly changes the fuel concentration gradient such that the OMLF changes its mode from a tribrachial flame mode (decreasing edge speed with fuel concentration gradient) to the premixed flame-like transition mode when the fuel concentration gradient becomes very small (increasing edge speed with fuel concentration gradient). Again, a tribrachial flame mode is recovered during a rising period of flame edge and repeats an oscillation cycle. (c) 2020 The Combustion Institute. Published by Elsevier Inc. All rights reserved. -
dc.identifier.bibliographicCitation PROCEEDINGS OF THE COMBUSTION INSTITUTE, v.38, no.2, pp.2049 - 2056 -
dc.identifier.doi 10.1016/j.proci.2020.06.355 -
dc.identifier.issn 1540-7489 -
dc.identifier.scopusid 2-s2.0-85091023783 -
dc.identifier.uri https://scholarworks.unist.ac.kr/handle/201301/48091 -
dc.identifier.url https://www.sciencedirect.com/science/article/pii/S154074892030448X?via%3Dihub -
dc.identifier.wosid 000651831800016 -
dc.language 영어 -
dc.publisher ELSEVIER SCIENCE INC -
dc.title On the oscillating flame characteristics in nonpremixed laminar coflow-jets: An experimental and numerical study -
dc.type Article -
dc.description.isOpenAccess FALSE -
dc.relation.journalWebOfScienceCategory Thermodynamics; Energy & Fuels; Engineering, Chemical; Engineering, Mechanical -
dc.relation.journalResearchArea Thermodynamics; Energy & Fuels; Engineering -
dc.type.docType Article -
dc.description.journalRegisteredClass scie -
dc.description.journalRegisteredClass scopus -
dc.subject.keywordAuthor Positive -
dc.subject.keywordAuthor negative buoyancy -
dc.subject.keywordAuthor Fuel concentration gradient -
dc.subject.keywordAuthor Oscillating lifted flame -
dc.subject.keywordAuthor Tribrachial lifted flame -
dc.subject.keywordPlus STABILIZATION MECHANISM -
dc.subject.keywordPlus TRIBRACHIAL FLAMES -
dc.subject.keywordPlus LIFTED FLAMES -
dc.subject.keywordPlus PROPAGATION -

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