Numerical simulations of annular jet impingement behaviour

3-dimensional numerical simulations for an annular jet of Re = 2500 on a flat impingement plate at separation distances of 1Do, 2Do, and 4Do were conducted. Steady-state SST k-ω RANS and transient WALE LES turbulence models were used. The simulated flow profiles show good agreement with experimental...

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主要作者: Teng, Justin Jia Ding
其他作者: New Tze How Daniel
格式: Final Year Project
語言:English
出版: 2017
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在線閱讀:http://hdl.handle.net/10356/73036
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機構: Nanyang Technological University
語言: English
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spelling sg-ntu-dr.10356-730362023-03-04T18:59:34Z Numerical simulations of annular jet impingement behaviour Teng, Justin Jia Ding New Tze How Daniel School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics 3-dimensional numerical simulations for an annular jet of Re = 2500 on a flat impingement plate at separation distances of 1Do, 2Do, and 4Do were conducted. Steady-state SST k-ω RANS and transient WALE LES turbulence models were used. The simulated flow profiles show good agreement with experimental observations, while further predicting regions of turbulence generation and mixing behaviour around the recirculation and impingement regions. The annular jet becomes asymmetrical and large-scale coherent structures dissipate beyond x/Do > 2, at which point transient numerical simulations facilitated the observation and analysis of smaller vortex structures otherwise undetectable by current experimental techniques. Spectral analysis of the jet axial velocity reveals three frequencies of oscillations with Sti = 0.068, 0.23, and 0.45. Bachelor of Engineering (Aerospace Engineering) 2017-12-22T04:23:10Z 2017-12-22T04:23:10Z 2017 Final Year Project (FYP) http://hdl.handle.net/10356/73036 en Nanyang Technological University 78 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering::Aerodynamics
spellingShingle DRNTU::Engineering::Aeronautical engineering::Aerodynamics
Teng, Justin Jia Ding
Numerical simulations of annular jet impingement behaviour
description 3-dimensional numerical simulations for an annular jet of Re = 2500 on a flat impingement plate at separation distances of 1Do, 2Do, and 4Do were conducted. Steady-state SST k-ω RANS and transient WALE LES turbulence models were used. The simulated flow profiles show good agreement with experimental observations, while further predicting regions of turbulence generation and mixing behaviour around the recirculation and impingement regions. The annular jet becomes asymmetrical and large-scale coherent structures dissipate beyond x/Do > 2, at which point transient numerical simulations facilitated the observation and analysis of smaller vortex structures otherwise undetectable by current experimental techniques. Spectral analysis of the jet axial velocity reveals three frequencies of oscillations with Sti = 0.068, 0.23, and 0.45.
author2 New Tze How Daniel
author_facet New Tze How Daniel
Teng, Justin Jia Ding
format Final Year Project
author Teng, Justin Jia Ding
author_sort Teng, Justin Jia Ding
title Numerical simulations of annular jet impingement behaviour
title_short Numerical simulations of annular jet impingement behaviour
title_full Numerical simulations of annular jet impingement behaviour
title_fullStr Numerical simulations of annular jet impingement behaviour
title_full_unstemmed Numerical simulations of annular jet impingement behaviour
title_sort numerical simulations of annular jet impingement behaviour
publishDate 2017
url http://hdl.handle.net/10356/73036
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