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dc.contributor.authorChang, Wen-Kueien_US
dc.contributor.authorChen, Chiun-Hsunen_US
dc.date.accessioned2014-12-08T15:15:10Z-
dc.date.available2014-12-08T15:15:10Z-
dc.date.issued2007en_US
dc.identifier.issn0010-2202en_US
dc.identifier.urihttp://hdl.handle.net/11536/11399-
dc.identifier.urihttp://dx.doi.org/10.1080/00102200701484316en_US
dc.description.abstractThe ignition delay and subsequent downward flame spread over a finite-length PMMA slab with the effect of radiation included in a two-dimensional wind tunnel are investigated using the opposed flow velocity as a parameter. The gas and solid phase temperatures, preheat length and heat flux are considered in order to examine the flame ignition and spread characteristics. The numerical results reveal that the ignition delay time increases with the opposed flow velocity. However, the flame spread rate varies with the opposed flow velocity in a non-monotonic manner that can be identified as two distinct regimes with a peak value in between. The flame spread rate reaches a maximum at V-g = 32 cm/s, and then falls, regardless of whether the flow velocity is increasing or decreasing. For V-g < 32 cm/s, the flame behaviors are dominated by oxygen transport. For V-g > 32 cm/s, the flame stretch effect controls the flame behavior. Additionally, this work demonstrates that the effect of radiation delays the flame ignition and reduces both the flame strength and the corresponding spread rate. The effects of the opposed flow temperature and thickness of the solid fuel are also investigated. The predicted results indicate that a higher opposed flow temperature or a thinner solid fuel facilitates the ignition and accelerates flame spread. The effect of opposed flow velocity eventually overcomes that of opposed flow temperature as the flow speed is further increased.en_US
dc.language.isoen_USen_US
dc.subjectdownward flame spreaden_US
dc.subjectignition delayen_US
dc.subjectopposed flow velocityen_US
dc.subjectradiation effecten_US
dc.titleEffect of opposed flow on flame spread over a finite-length PMMA slab in a two-dimensional wind tunnelen_US
dc.typeArticleen_US
dc.identifier.doi10.1080/00102200701484316en_US
dc.identifier.journalCOMBUSTION SCIENCE AND TECHNOLOGYen_US
dc.citation.volume179en_US
dc.citation.issue12en_US
dc.citation.spage2489en_US
dc.citation.epage2510en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000251240000003-
dc.citation.woscount0-
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