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contributor authorHuang, Szu
contributor authorLiu, Yao
date accessioned2017-05-09T01:02:54Z
date available2017-05-09T01:02:54Z
date issued2013
identifier issn1948-5085
identifier othertsea_005_04_041003.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153253
description abstractHeat transfer in a leading edge, triangularshaped cooling channel with three channel orientations under high rotation numbers is investigated in this study. Continuous ribs and Vshaped ribs (P/e = 9, e/Dh = 0.085), both placed at an angle (خ±â€‰= 45 deg) to the mainstream flow, are applied on the leading and trailing surfaces. The Reynolds number range is 15,000–25,000 and the rotation number range is 0–0.65. Effects of high rotation number on heat transfer with three angles of rotation (90 deg, 67.5 deg, and 45 deg) are tested. Results show that heat transfer is influenced by the combined effects of rib and channel orientation. When the rotation number is smaller than 0.4, rotation causes a decrease in the average Nusselt number ratios on the leading surface at a channel orientation of 90 deg. Heat transfer is enhanced gradually on the leading surface when the channel orientation varies from 90 deg to 45 deg for both ribbed cases. The highest heat transfer enhancement due to rotation is found at the highest rotation number of 0.65.
publisherThe American Society of Mechanical Engineers (ASME)
titleHigh Rotation Number Effect on Heat Transfer in a Leading Edge Cooling Channel of Gas Turbine Blades With Three Channel Orientations
typeJournal Paper
journal volume5
journal issue4
journal titleJournal of Thermal Science and Engineering Applications
identifier doi10.1115/1.4023888
journal fristpage41003
journal lastpage41003
identifier eissn1948-5093
treeJournal of Thermal Science and Engineering Applications:;2013:;volume( 005 ):;issue: 004
contenttypeFulltext


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