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dc.contributor.authorYang, Xiang IA
dc.contributor.authorJariwala, Vishal
dc.contributor.authorXu, Haosen HA
dc.contributor.authorLarosiliere, Louis
dc.date.accessioned2022-05-08T08:54:01Z
dc.date.available2022-05-08T08:54:01Z
dc.date.copyright10/1/2021 12:00:00 AM
dc.date.issued2021
dc.identifier.issn0889-504X
dc.identifier.otherturbo_144_3_031004.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4284483
dc.description.abstractIn analogy with the classical concept of mass-flux-based streamlines, we define angular momentum transport (AMT) lines as an aerodynamic functional diagnostic tool. The AMT lines are the ones whose tangents are given by the average angular momentum flux. The mathematical and physical properties of these AMT lines are exploited to study the generation, removal, and transport of angular momentum in turbomachinery components. We illustrate the concept by visualizing AMT lines in two relatively simple flows, namely, vaneless incompressible diffuser and von Karman flow (a model of centrifugal compressors). Next, we apply the proposed diagnostic tool to flow in a return channel. A return channel is a part of a multistage centrifugal compressor stage. Its principal function is to remove angular momentum. In this work, we apply the diagnostic tool of AMT lines to a Reynolds-averaged Navier Stokes (RANS) simulation and a wall-modeled large eddy simulation (LES) of flow in the return channel. We show that AMT lines give us insights into the AMT process that are otherwise not available with conventional visualization tools.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleAerodynamic Functional Diagnostics Based on Angular Momentum Transport Lines
dc.typeJournal Paper
dc.journal.volume144
dc.journal.issue3
dc.journal.titleJournal of Turbomachinery
dc.identifier.doi10.1115/1.4052354
dc.journal.fristpage31004-1
dc.journal.lastpage31004-8
dc.page8
dc.treeJournal of Turbomachinery:;2021:;volume( 144 ):;issue: 003
dc.contenttypeFulltext


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