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contributor authorBarringer, Michael
contributor authorThole, Karen A.
contributor authorKrishnan, Vaidyanathan
contributor authorLandrum, Evan
date accessioned2017-05-09T01:13:34Z
date available2017-05-09T01:13:34Z
date issued2014
identifier issn0889-504X
identifier otherturbo_136_05_051012.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156594
description abstractVariations from manufacturing can influence the overall pressure drop and subsequent flow rates through supply holes in such applications as filmcooling, transpiration cooling, and impingement cooling that are supplied by microchannels, pipeflow systems, or secondary air systems. The inability to accurately predict flow rates has profound effects on engine operations. The objective of this study was to investigate the influence of several relevant manufacturing features that might occur for a cooling supply hole being fed by a range of channel configurations. The manufacturing variances included the ratio of the hole diameter to the channel width, the number of channel feeds (segments), the effect of hole overlap with respect to the channel sidewalls, and the channel Reynolds number. The results showed that the friction factors for the typically long channels in this study were independent of the tested inlet and exit hole configurations. The results also showed that the nondimensional pressure loss coefficients for the flow passing through the channel inlet holes and through the channel exit holes were found to be independent of the channel flow Reynolds number over the tested range. The geometric scaling ratio of the hole crosssectional area to the channel crosssectional area collapsed the pressure loss coefficients the best for both one and two flow segments for both the channel inlet and channel exit hole.
publisherThe American Society of Mechanical Engineers (ASME)
titleManufacturing Influences on Pressure Losses of Channel Fed Holes
typeJournal Paper
journal volume136
journal issue5
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4025226
journal fristpage51012
journal lastpage51012
identifier eissn1528-8900
treeJournal of Turbomachinery:;2014:;volume( 136 ):;issue: 005
contenttypeFulltext


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