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contributor authorS. Acharya
contributor authorV. Eliades
contributor authorD. E. Nikitopoulos
date accessioned2017-05-09T00:06:20Z
date available2017-05-09T00:06:20Z
date copyrightJanuary, 2001
date issued2001
identifier issn0889-504X
identifier otherJOTUEI-28686#97_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126085
description abstractThe effects of ribs with different cross-stream profiles are investigated through detailed, surface mass (heat) transfer distributions along four active walls of a square duct containing a sharp 180 deg bend. The duct simulates two passes of an internal coolant channel in a gas turbine engine with ribs mounted on two opposite walls. Mass (heat) transfer measurements, taken using the naphthalene sublimation technique, are presented for a Reynolds number of 30,000, and rotation number of 0.3. Comparisons are made with conventional ribs having a rectangular cross section. It is shown that the use of certain profiled ribs provides considerable heat transfer enhancements over conventional ribs with the same blockage ratio in the duct. These enhancements are attributed to the generation of longitudinal vorticity (or secondary flows) by the profiled ribs in the channel.
publisherThe American Society of Mechanical Engineers (ASME)
titleHeat Transfer Enhancements in Rotating Two-Pass Coolant Channels With Profiled Ribs: Part 1–Average Results
typeJournal Paper
journal volume123
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1331539
journal fristpage97
journal lastpage106
identifier eissn1528-8900
keywordsHeat transfer
keywordsChannels (Hydraulic engineering)
keywordsFlow (Dynamics)
keywordsCoolants
keywordsDucts
keywordsMass transfer
keywordsHeat
keywordsMeasurement AND Reynolds number
treeJournal of Turbomachinery:;2001:;volume( 123 ):;issue: 001
contenttypeFulltext


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