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dc.contributor.authorTsui, YYen_US
dc.contributor.authorLu, CYen_US
dc.date.accessioned2014-12-08T15:17:32Z-
dc.date.available2014-12-08T15:17:32Z-
dc.date.issued2006-01-20en_US
dc.identifier.issn0271-2091en_US
dc.identifier.urihttp://dx.doi.org/10.1002/fld.1052en_US
dc.identifier.urihttp://hdl.handle.net/11536/12724-
dc.description.abstractA numerical method is employed to examine the now in symmetrical, two-dimensional branches of Y shape and Tee shape. The methodology is based oil a pressure-correction procedure within the frame of unstructured grids. Specified pressures are imposed at the outlets of the two branches. The area ratio of the branch is allowed to vary in the range of 2-3. Separation of the flow in the bifurcating region is inevitable. Willi equal Millet pressures, symmetrical flow patterns prevail except for the Y type branch Under the conditions of high Reynolds numbers and large area ratios. This implies that the Y-branch flow is more sensitive to small disturbances. It is shown that with a slightly higher pressure imposed oil one of the two branches the structure Of the recirculating flow for the Y type is greatly affected and the flow rate is reduced dramatically in the high-pressure branch channel. In contrast, the influence on the Tee type branch is much lower since the flow behaves like a jet impinging oil a confined duct. Copyright (c) 2005 John Wiley & Sons, Ltd.en_US
dc.language.isoen_USen_US
dc.subjectbranching flowsen_US
dc.subjectrecirculating vorticesen_US
dc.subjectsymmetry breakingen_US
dc.subjectpressure boundary conditionsen_US
dc.subjectunstructured gridsen_US
dc.titleA study of the recirculating flow in planar, symmetrical branching channelsen_US
dc.typeArticleen_US
dc.identifier.doi10.1002/fld.1052en_US
dc.identifier.journalINTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDSen_US
dc.citation.volume50en_US
dc.citation.issue2en_US
dc.citation.spage235en_US
dc.citation.epage253en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000234442900006-
dc.citation.woscount5-
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