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dc.contributor.authorYen, Hung-Chengen_US
dc.contributor.authorHsu, Wen-Syangen_US
dc.contributor.authorHuang, Jeng-Minen_US
dc.contributor.authorLu, Chi-Wenen_US
dc.contributor.authorHsu, Chin-Nanen_US
dc.date.accessioned2015-07-21T08:29:09Z-
dc.date.available2015-07-21T08:29:09Z-
dc.date.issued2015-04-01en_US
dc.identifier.issn0334-0082en_US
dc.identifier.urihttp://dx.doi.org/10.1515/tjj-2014-0018en_US
dc.identifier.urihttp://hdl.handle.net/11536/124688-
dc.description.abstractAn in-line tube fan with design flow rate 1 m(3)/s, static pressure 1030 Pa, rotation speed 3450 rpm, and specific speed 2.1 was investigated. Inverse design method was used to design deswirl vane while CFD to analyze its flow field. Results showed that although the efficiency of the axial straight flat plate is poor, it remained better than that of the vaneless type. The efficiency of deswirl vane was much higher than the previous two. However, when the casing-impeller ratio was lower than 1.25, completely recovering tangential velocity would result in large recirculation flow near outlet of deswirl vane. When the casing-impeller ratio increased to 1.33, the recirculation flow and pressure loss were obviously reduced. When the casing-impeller ratio increased to 1.46, the deswirl vane almost completely recovered tangential velocity, and pressure loss was further reduced. Static pressure and efficiency at operating point were 10% and 6% higher than the casing-impeller ratio 1.33.en_US
dc.language.isoen_USen_US
dc.subjectin-line tube fanen_US
dc.subjectdeswirl vaneen_US
dc.subjectCFDen_US
dc.subjectperformance testingen_US
dc.titleDevelopment of a High Efficiency In-Line Tube Fan Using CFDen_US
dc.typeArticleen_US
dc.identifier.doi10.1515/tjj-2014-0018en_US
dc.identifier.journalINTERNATIONAL JOURNAL OF TURBO & JET-ENGINESen_US
dc.citation.volume32en_US
dc.citation.spage105en_US
dc.citation.epage115en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000354112700010en_US
dc.citation.woscount0en_US
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