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dc.contributor.authorWildgoose, Alexander J.
dc.contributor.authorThole, Karen A.
dc.date.accessioned2023-08-16T18:11:30Z
dc.date.available2023-08-16T18:11:30Z
dc.date.copyright2/10/2023 12:00:00 AM
dc.date.issued2023
dc.identifier.issn0889-504X
dc.identifier.otherturbo_145_7_071011.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4291588
dc.description.abstractAdditive manufacturing (AM) provides the ability to fabricate highly customized internal cooling passages that are relevant to gas turbine components. This experimental study examines the pressure loss and heat transfer performance of a range of fundamental channel shapes that were produced using direct metal laser sintering. Circular, hexagonal, pentagonal, elliptical, diamond, square, rectangular, trapezoidal, and triangular channel cross sections were investigated. To maintain the same convective surface area between shapes, the wetted perimeters of the channel cross sections were kept constant. Parallel computational fluid dynamic simulations were performed to understand the relationships in cooling performance between several channel shapes. Several characteristic length scales were evaluated to scale the pressure loss and heat transfer measurements. Among the channel shapes investigated, the diamond channel showed the lowest Nusselt number and friction factor. The pentagon exhibited a similar Nusselt number as the circular channel despite having a lower friction factor. There was no difference in scaling the friction factor or Nusselt number results of the different channel shapes between using the square root of cross-sectional area compared to hydraulic diameter as the characteristic length scale
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleHeat Transfer and Pressure Loss of Additively Manufactured Internal Cooling Channels With Various Shapes
dc.typeJournal Paper
dc.journal.volume145
dc.journal.issue7
dc.journal.titleJournal of Turbomachinery
dc.identifier.doi10.1115/1.4056775
dc.journal.fristpage71011-1
dc.journal.lastpage71011-11
dc.page11
dc.treeJournal of Turbomachinery:;2023:;volume( 145 ):;issue: 007
dc.contenttypeFulltext


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