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contributor authorHickling, Tom
contributor authorHe, Li
date accessioned2023-08-16T18:10:52Z
date available2023-08-16T18:10:52Z
date copyright12/13/2022 12:00:00 AM
date issued2022
identifier issn0889-504X
identifier otherturbo_145_6_061006.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4291567
description abstractThe flow and heat transfer within rotating cavities is often discussed as a conjugate problem; the temperature distribution within the cavity disks drives the large-scale flow structure within the cavity, and the cavity aerodynamics influence the heat transfer to the disks. However, most simulations of rotating cavities only consider the fluid domain in isolation. This is particularly true for turbulence resolving approaches such as large eddy simulation (LES). The large time-scale disparity between the fluid time-steps used in LES and the characteristic solid time-scale complicates the use of LES with conjugate heat transfer (CHT). A further issue is that an under-resolved solid mesh artificially amplifies higher frequency temperature fluctuations from the fluid. This paper addresses these challenges with a new method for LES-CHT where the low frequency temperature fluctuation caused by the large-scale flow structure is accounted for using a multi-scale frequency domain approach. We investigate two cases: axially heated disks made of a low conductivity material, and disks made from a higher conductivity material with a temperature set by radial conduction from the shroud. The formation of small-scale flow structures on both the disk and shroud is dependent on the heating configuration of the cavity—indicating that high-fidelity thermal boundary conditions should be used when simulating rotating cavities. The formation of heating induced vortical flow structures near the disk is particularly interesting, as this is unexpected from the laminar Ekman layer modeling argument usually used to consider this region.
publisherThe American Society of Mechanical Engineers (ASME)
titleLES-CHT for a Rotating Cavity With Axial Throughflow
typeJournal Paper
journal volume145
journal issue6
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4056091
journal fristpage61006-1
journal lastpage61006-12
page12
treeJournal of Turbomachinery:;2022:;volume( 145 ):;issue: 006
contenttypeFulltext


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