完整後設資料紀錄
DC 欄位語言
dc.contributor.authorHuang, Szu-Chien_US
dc.contributor.authorLiu, Yao-Hsienen_US
dc.date.accessioned2014-12-08T15:36:01Z-
dc.date.available2014-12-08T15:36:01Z-
dc.date.issued2012en_US
dc.identifier.isbn978-0-7918-4470-0en_US
dc.identifier.urihttp://hdl.handle.net/11536/24376-
dc.description.abstractHeat transfer in a leading edge, triangular shaped cooling channel with three channel orientations under high rotation numbers is experimentally studied. Continuous ribs and V-shaped ribs, both at 45 degrees rib angle of attack, are applied on the leading and trailing surfaces. For each rib case, three channel orientations (90 degrees, 67.5 degrees, and 45 degrees) with respect to the plane of rotation are tested. The rib height to hydraulic diameter ratio (e/D-h) is 0.085 and the rib pitch to height ratio (Pie) is 9. Reynolds numbers are from 15000 to 25000, and the rotation numbers are from 0 to 0.65. Results show that the heat transfer variation is influenced by the combined effects of rib configuration and channel orientation. Effect of channel orientation influences local heat transfer distribution inside this triangular channel, and heat transfer is enhanced gradually on the leading surface when the channel orientation varies from 90 to 45 for both ribbed cases in this study.en_US
dc.language.isoen_USen_US
dc.titleHIGH ROTATION NUMBER EFFECT ON HEAT TRANSFER IN A LEADING EDGE COOLING CHANNEL WITH THREE CHANNEL ORIENTATIONSen_US
dc.typeProceedings Paperen_US
dc.identifier.journalPROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 4, PTS A AND Ben_US
dc.citation.spage1289en_US
dc.citation.epage1298en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000335868900114-
顯示於類別:會議論文