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contributor authorSnyder, Jacob C.
contributor authorStimpson, Curtis K.
contributor authorThole, Karen A.
contributor authorMongillo, Dominic
date accessioned2017-05-09T01:34:08Z
date available2017-05-09T01:34:08Z
date issued2016
identifier issn0889-504X
identifier otherturbo_138_05_051006.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162765
description abstractWith the advance of direct metal laser sintering (DMLS), also generically referred to as additive manufacturing (AM), novel geometric features of internal channels for gas turbine cooling can be achieved beyond those features using traditional manufacturing techniques. There are many variables, however, in the DMLS process that affect the final quality of the part. Of most interest to gas turbine heat transfer designers are the roughness levels and tolerance levels that can be held for the internal channels. This study investigates the effect of DMLS build direction and channel shape on the pressure loss and heat transfer measurements of smallscale channels. Results indicate that differences in pressure loss occur between the test cases with differing channel shapes and build directions, while little change is measured in heat transfer performance.
publisherThe American Society of Mechanical Engineers (ASME)
titleBuild Direction Effects on Additively Manufactured Channels
typeJournal Paper
journal volume138
journal issue5
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4032168
journal fristpage51006
journal lastpage51006
identifier eissn1528-8900
treeJournal of Turbomachinery:;2016:;volume( 138 ):;issue: 005
contenttypeFulltext


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