RANS and hybrid LES/RANS simulations of flow over a square cylinder

Abstract Unsteady RANS (URANS), hybrid LES/RANS and IDDES simulations were conducted to numerically investigate the velocity field around, and pressures distribution and forces over a square cylinder immersed in a uniform, steady oncoming flow with Reynolds number Re = 21,400. The vortex shedding re...

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Main Author: Jianghua Ke
Format: Article
Language:English
Published: SpringerOpen 2019-05-01
Series:Advances in Aerodynamics
Subjects:
Online Access:http://link.springer.com/article/10.1186/s42774-019-0012-9
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spelling doaj-85b44f68058c4c42b274d4f2c7d3939c2020-11-25T02:10:35ZengSpringerOpenAdvances in Aerodynamics2524-69922019-05-011112410.1186/s42774-019-0012-9RANS and hybrid LES/RANS simulations of flow over a square cylinderJianghua Ke0National Institute of Standards and TechnologyAbstract Unsteady RANS (URANS), hybrid LES/RANS and IDDES simulations were conducted to numerically investigate the velocity field around, and pressures distribution and forces over a square cylinder immersed in a uniform, steady oncoming flow with Reynolds number Re = 21,400. The vortex shedding responses in terms of Strouhal number, the pressure distribution, the velocity profile and the velocity fluctuations obtained by numerical simulations are compared with experimental data. Compared with 2D URANS simulation, 3D simulations using hybrid LES/RANS and IDDES models provide more accurate prediction on the responses in the wake, including mean streamwise velocity profile and rms velocity fluctuations. This also results in more accurate prediction of time-averaged surface pressure coefficient on the rear surface obtained by 3D hybrid LES/RANS and IDDES simulations than by URANS simulation. When a hybrid LES/RANS model or IDDES model is used, a more accurate prediction for either pressure coefficient or velocity profile (especially in the far wake region) is not guaranteed by increasing the mesh resolution along the spanwise direction of the square cylinder.http://link.springer.com/article/10.1186/s42774-019-0012-9URANSHybrid LES/RANSIDDESSquare cylinderTurbulence modeling
collection DOAJ
language English
format Article
sources DOAJ
author Jianghua Ke
spellingShingle Jianghua Ke
RANS and hybrid LES/RANS simulations of flow over a square cylinder
Advances in Aerodynamics
URANS
Hybrid LES/RANS
IDDES
Square cylinder
Turbulence modeling
author_facet Jianghua Ke
author_sort Jianghua Ke
title RANS and hybrid LES/RANS simulations of flow over a square cylinder
title_short RANS and hybrid LES/RANS simulations of flow over a square cylinder
title_full RANS and hybrid LES/RANS simulations of flow over a square cylinder
title_fullStr RANS and hybrid LES/RANS simulations of flow over a square cylinder
title_full_unstemmed RANS and hybrid LES/RANS simulations of flow over a square cylinder
title_sort rans and hybrid les/rans simulations of flow over a square cylinder
publisher SpringerOpen
series Advances in Aerodynamics
issn 2524-6992
publishDate 2019-05-01
description Abstract Unsteady RANS (URANS), hybrid LES/RANS and IDDES simulations were conducted to numerically investigate the velocity field around, and pressures distribution and forces over a square cylinder immersed in a uniform, steady oncoming flow with Reynolds number Re = 21,400. The vortex shedding responses in terms of Strouhal number, the pressure distribution, the velocity profile and the velocity fluctuations obtained by numerical simulations are compared with experimental data. Compared with 2D URANS simulation, 3D simulations using hybrid LES/RANS and IDDES models provide more accurate prediction on the responses in the wake, including mean streamwise velocity profile and rms velocity fluctuations. This also results in more accurate prediction of time-averaged surface pressure coefficient on the rear surface obtained by 3D hybrid LES/RANS and IDDES simulations than by URANS simulation. When a hybrid LES/RANS model or IDDES model is used, a more accurate prediction for either pressure coefficient or velocity profile (especially in the far wake region) is not guaranteed by increasing the mesh resolution along the spanwise direction of the square cylinder.
topic URANS
Hybrid LES/RANS
IDDES
Square cylinder
Turbulence modeling
url http://link.springer.com/article/10.1186/s42774-019-0012-9
work_keys_str_mv AT jianghuake ransandhybridlesranssimulationsofflowoverasquarecylinder
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