A numerical investigation on flow past skewed vortex generators ahead of a backward facing ramp

Flow past a backward facing ramp (BFR) with rectangular vane-type vortex generators (VGs) located upstream has been studied numerically using OpenFOAM based steady-state RANS simulations. In particular, single and multiple pair(s) of boundary layer height VGs are skewed at 10° and 30° to study their...

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Main Authors: Cheawchan, Atcha-uea, Mohamed Arif Mohamed, Ng, Bing Feng, New, Tze How
其他作者: School of Mechanical and Aerospace Engineering
格式: Article
語言:English
出版: 2022
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在線閱讀:https://hdl.handle.net/10356/161671
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機構: Nanyang Technological University
語言: English
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spelling sg-ntu-dr.10356-1616712022-09-14T03:04:20Z A numerical investigation on flow past skewed vortex generators ahead of a backward facing ramp Cheawchan, Atcha-uea Mohamed Arif Mohamed Ng, Bing Feng New, Tze How School of Mechanical and Aerospace Engineering Engineering::Aeronautical engineering Flow Separation Vortex Generators Flow past a backward facing ramp (BFR) with rectangular vane-type vortex generators (VGs) located upstream has been studied numerically using OpenFOAM based steady-state RANS simulations. In particular, single and multiple pair(s) of boundary layer height VGs are skewed at 10° and 30° to study their effects on the flow separation behaviour at Re=3×106. Streamwise and cross-stream results show that single VGs produce counter-rotating streamwise vortices with increasingly different vortex-core strengths and vortical interactions when skewness angle increases. At 30° however, co-rotating vortices are formed instead with significantly heightened vortical interaction levels, leading to asymmetric flow separation and reattachment behaviour. In particular, the use of multiple VGs under the same condition further accentuate these behaviour and results in significant changes to the wall shear stress distribution. Clarifications on how the flow separation region is distorted by the symmetric/asymmetric streamwise vortices based on velocity component analysis are also provided. Lastly, trajectories of the streamwise vortices and vortex-core characteristics support the notion that the streamwise vortices behave significantly more non-linearly at 30° skewness angle here, and that skewing the present VGs such that they produce co-rotating vortices instead of counter-rotating ones leads to very different flow separation control characteristics. Submitted/Accepted version 2022-09-14T03:04:20Z 2022-09-14T03:04:20Z 2022 Journal Article Cheawchan, A., Mohamed Arif Mohamed, Ng, B. F. & New, T. H. (2022). A numerical investigation on flow past skewed vortex generators ahead of a backward facing ramp. Aerospace Science and Technology, 123, 107435-. https://dx.doi.org/10.1016/j.ast.2022.107435 1270-9638 https://hdl.handle.net/10356/161671 10.1016/j.ast.2022.107435 2-s2.0-85125693417 123 107435 en Aerospace Science and Technology © 2022 Elsevier Masson SAS. All rights reserved. This paper was published in Aerospace Science and Technology and is made available with permission of Elsevier Masson SAS. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Aeronautical engineering
Flow Separation
Vortex Generators
spellingShingle Engineering::Aeronautical engineering
Flow Separation
Vortex Generators
Cheawchan, Atcha-uea
Mohamed Arif Mohamed
Ng, Bing Feng
New, Tze How
A numerical investigation on flow past skewed vortex generators ahead of a backward facing ramp
description Flow past a backward facing ramp (BFR) with rectangular vane-type vortex generators (VGs) located upstream has been studied numerically using OpenFOAM based steady-state RANS simulations. In particular, single and multiple pair(s) of boundary layer height VGs are skewed at 10° and 30° to study their effects on the flow separation behaviour at Re=3×106. Streamwise and cross-stream results show that single VGs produce counter-rotating streamwise vortices with increasingly different vortex-core strengths and vortical interactions when skewness angle increases. At 30° however, co-rotating vortices are formed instead with significantly heightened vortical interaction levels, leading to asymmetric flow separation and reattachment behaviour. In particular, the use of multiple VGs under the same condition further accentuate these behaviour and results in significant changes to the wall shear stress distribution. Clarifications on how the flow separation region is distorted by the symmetric/asymmetric streamwise vortices based on velocity component analysis are also provided. Lastly, trajectories of the streamwise vortices and vortex-core characteristics support the notion that the streamwise vortices behave significantly more non-linearly at 30° skewness angle here, and that skewing the present VGs such that they produce co-rotating vortices instead of counter-rotating ones leads to very different flow separation control characteristics.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Cheawchan, Atcha-uea
Mohamed Arif Mohamed
Ng, Bing Feng
New, Tze How
format Article
author Cheawchan, Atcha-uea
Mohamed Arif Mohamed
Ng, Bing Feng
New, Tze How
author_sort Cheawchan, Atcha-uea
title A numerical investigation on flow past skewed vortex generators ahead of a backward facing ramp
title_short A numerical investigation on flow past skewed vortex generators ahead of a backward facing ramp
title_full A numerical investigation on flow past skewed vortex generators ahead of a backward facing ramp
title_fullStr A numerical investigation on flow past skewed vortex generators ahead of a backward facing ramp
title_full_unstemmed A numerical investigation on flow past skewed vortex generators ahead of a backward facing ramp
title_sort numerical investigation on flow past skewed vortex generators ahead of a backward facing ramp
publishDate 2022
url https://hdl.handle.net/10356/161671
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