Show simple item record

contributor authorS. Mochizuki
contributor authorA. Murata
contributor authorM. Fukunaga
date accessioned2017-05-08T23:55:07Z
date available2017-05-08T23:55:07Z
date copyrightJuly, 1997
date issued1997
identifier issn0889-504X
identifier otherJOTUEI-28661#610_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119614
description abstractThe objective of this study was to investigate, through experiments, the combined effects of a sharp 180 deg turn and rib patterns on the pressure drop performance and distributions of the local heat transfer coefficient in an entire two-pass rib-roughened channel with a 180 deg turn. The rib pitch-to-equivalent diameter ratio P/de was 1.0, the rib-height-to-equivalent diameter ratio e/de was 0.09, and the rib angle relative to the main flow direction was varied from 30 ∼ 90 deg with an interval of 15 deg. Experiments were conducted for Reynolds numbers in the range 4000 ∼ 30,000. It was disclosed that, due to the interactions between the bend-induced secondary flow and the rib-induced secondary flow, the combination of rib patterns in the channel before and after the turn causes considerable differences in the pressure drop and heat transfer performance of the entire channel.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffects of Rib Arrangements on Pressure Drop and Heat Transfer in a Rib-Roughened Channel With a Sharp 180 deg Turn
typeJournal Paper
journal volume119
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2841165
journal fristpage610
journal lastpage616
identifier eissn1528-8900
keywordsHeat transfer
keywordsChannels (Hydraulic engineering)
keywordsPressure drop
keywordsFlow (Dynamics)
keywordsHeat transfer coefficients AND Reynolds number
treeJournal of Turbomachinery:;1997:;volume( 119 ):;issue: 003
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record