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dc.contributor.authorTsui, Yeng-Yungen_US
dc.contributor.authorLin, Shih-Chaoen_US
dc.contributor.authorShen, Shih-Jhenen_US
dc.contributor.authorHu, Yu-Changen_US
dc.date.accessioned2014-12-08T15:12:55Z-
dc.date.available2014-12-08T15:12:55Z-
dc.date.issued2008en_US
dc.identifier.issn1040-7782en_US
dc.identifier.urihttp://hdl.handle.net/11536/9960-
dc.identifier.urihttp://dx.doi.org/10.1080/10407780701790102en_US
dc.description.abstractIn this study we are concerned with the flow in a tank stirred by disc impellers with pitched blades. A mathematical method, based on multiframe of reference and unstructured grid technology, was employed in the flow simulation. It was learned from the study by Tsui et al. [12] that for a pitched-blade impeller, which does not include the disc, the flow pattern in the agitated tank is transformed from the axial type to the radial type at a particular angle when the blade angle is increased. A similar phenomenon was observed in the present study. However, in contrast to the results of Tsui et al., the change of flow pattern brings about a sharp decrease in power requirement and a jump in pumping capacity. The cause of the difference is related to the disc which obstructs the fluid when it flows in the axial direction at low blade angles and makes it flow smoothly in the radial direction along the disc at high blade angles. It was shown in the results that the transition angle is increased when the impeller size, the disc size as well as the off-bottom clearance are reduced.en_US
dc.language.isoen_USen_US
dc.titleAnalysis of the flow agitated by disc impellers with pitched bladesen_US
dc.typeArticleen_US
dc.identifier.doi10.1080/10407780701790102en_US
dc.identifier.journalNUMERICAL HEAT TRANSFER PART A-APPLICATIONSen_US
dc.citation.volume53en_US
dc.citation.issue10en_US
dc.citation.spage1091en_US
dc.citation.epage1108en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000252352300005-
dc.citation.woscount1-
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