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contributor authorHickling, Tom
contributor authorHe, Li
date accessioned2022-02-05T22:20:50Z
date available2022-02-05T22:20:50Z
date copyright2/26/2021 12:00:00 AM
date issued2021
identifier issn0742-4795
identifier othergtp_143_04_041014.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4277375
description abstractAcross the open literature, there is no clear consensus on what the most suitable modeling fidelity is for rotating cavity flows. Although it is a widely held opinion that unsteady Reynolds-averaged-Navier–Stokes (URANS) approaches are unsuitable, many authors have succeeded in getting reasonable heat transfer results with them. There is also a lack of research into the validity of hybrid URANS/large eddy simulation (LES) type approaches such as detached eddy simulation (DES). This paper addresses these research challenges with a systematic investigation of a rotating cavity with axial throughflow at Grashof numbers of 3.03×109 and 3.03×1011. The disk near-wall layers remained laminar at both conditions, meaning that a turbulence model should not be active in these regions. The disk heat transfer was observed to affect the near-disk aerodynamics, which in turn affect the disk heat transfer: this feedback loop implies that conjugate heat transfer computations of rotating cavities may be worth investigating. On the shroud, additional eddy viscosity in URANS and DES was found to interfere with the formation of heat transfer enhancing streaks, whilst these were always captured by LES. DES exhibited a concerning behavior at the higher Grashof number. Locally generated eddy viscosity from the shroud was injected into the bulk fluid by the radial inflow. This contaminated the entire cavity with nonphysical modeled turbulence. As the radial inflow is a characteristic feature of rotating cavity flows, these results show that caution is necessary when applying hybrid URANS/LES approaches to this type of flow.
publisherThe American Society of Mechanical Engineers (ASME)
titleSome Observations on the Computational Sensitivity of Rotating Cavity Flows
typeJournal Paper
journal volume143
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4049824
journal fristpage041014-1
journal lastpage041014-12
page12
treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 004
contenttypeFulltext


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