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dc.contributor.authorTsui, YYen_US
dc.contributor.authorWang, CKen_US
dc.date.accessioned2014-12-08T15:03:04Z-
dc.date.available2014-12-08T15:03:04Z-
dc.date.issued1995-12-01en_US
dc.identifier.issn0098-2202en_US
dc.identifier.urihttp://hdl.handle.net/11536/1645-
dc.description.abstractThis study is concerned with numerical analysis of laminar separated flow in symmetric, two-dimensional, straight-walled diffusers. With Reynolds numbers Re = 56 and 114 and expansion ratios ER = 3 and 4, totally, there are four cases considered. At the low Reynolds number and the low expansion reaction the flow in the diffuser is nearly symmetric to the center line, irrespective of the diffusion angle. As Reynolds number or expansion ratio increases, a large recirculation region forms at one side wall and a small one at the other side. For the case with Re = 114 and ER = 4 the small recirculating flow disappears at small diffusion angles and a third recirculating flow appear in the same side of the small main recirculation region for large diffusion angles. The pressure recovery reaches its peak value somewhere downstream of the reattachment point of the large recirculating flow. The effectiveness of the diffuser deteriorates as the diffusion angle increases, apart from that at Re = 56 the effectiveness increases from theta = 15 to 30 deg. Symmetric flow solutions can be obtained by incorporating a symmetric relaxation method. The pressure recovery is higher for the symmetric flow than that for the asymmetric flow owing to the weaker recirculating strength in the former.en_US
dc.language.isoen_USen_US
dc.titleCalculation of laminar separated flow in symmetric two dimensional diffusersen_US
dc.typeArticleen_US
dc.identifier.journalJOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASMEen_US
dc.citation.volume117en_US
dc.citation.issue4en_US
dc.citation.spage612en_US
dc.citation.epage616en_US
dc.contributor.department交大名義發表zh_TW
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentNational Chiao Tung Universityen_US
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:A1995TY06900013-
dc.citation.woscount23-
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