A numerical simulation study on vortex-ring collisions upon arbitrary solid boundary

In this study, vortex behaviour near to complex geometry was investigated experimentally and numerically by studying the collision of a Re 2000 vortex ring upon V-shaped plates with 30, 60, 90 degrees vertices. Normal collision of vortex ring upon flat wall was also simulated using large eddy simula...

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Main Author: Leong, Sheng Yuan
Other Authors: New Tze How Daniel
Format: Final Year Project
Language:English
Published: 2018
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Online Access:http://hdl.handle.net/10356/74516
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-745162023-03-04T18:16:06Z A numerical simulation study on vortex-ring collisions upon arbitrary solid boundary Leong, Sheng Yuan New Tze How Daniel School of Mechanical and Aerospace Engineering DRNTU::Engineering In this study, vortex behaviour near to complex geometry was investigated experimentally and numerically by studying the collision of a Re 2000 vortex ring upon V-shaped plates with 30, 60, 90 degrees vertices. Normal collision of vortex ring upon flat wall was also simulated using large eddy simulation (LES). The numerical results showed that LES is capable in predicting important vortex features qualitatively. The results of vortex ring colliding upon V-plates showed that the transverse ends of vortex ring, which collided earlier with the wall, induced secondary vortex and entrained it rapidly accompanied with significant reduction of core’s size. This phenomenon is similar to the lower core of vortex ring in oblique collision upon a flat wall. Other part of vortex ring collided with the wall subsequently and induced secondary vortex at different locations and times. Due to the decreasing transverse spacing in the V-shaped groove, azimuthal instabilities developed on primary and secondary vortices. The azimuthal waviness was compressed and displaced toward the longitudinal plane. It was followed by intense self-interaction and three-dimensional vortex stretching between the azimuthal waviness. The entire vortex structure was then stretched longitudinally with the production small scale hairpin vortices. It was found that the greater the vertex angle, the weaker shearing action experienced by the primary vortex. It resulted in stronger induction of boundary layer and secondary vortices which led to more intense interaction between primary and secondary vortex. However, the interaction between boundary layer and small scale hairpin vortices still remain unclear due to its complicated and three-dimensional nature. Future research can be conducted to understand more about the formation and breakdown of small scale vortices at the near-wall region. Bachelor of Engineering (Aerospace Engineering) 2018-05-21T03:47:34Z 2018-05-21T03:47:34Z 2018 Final Year Project (FYP) http://hdl.handle.net/10356/74516 en Nanyang Technological University 74 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
spellingShingle DRNTU::Engineering
Leong, Sheng Yuan
A numerical simulation study on vortex-ring collisions upon arbitrary solid boundary
description In this study, vortex behaviour near to complex geometry was investigated experimentally and numerically by studying the collision of a Re 2000 vortex ring upon V-shaped plates with 30, 60, 90 degrees vertices. Normal collision of vortex ring upon flat wall was also simulated using large eddy simulation (LES). The numerical results showed that LES is capable in predicting important vortex features qualitatively. The results of vortex ring colliding upon V-plates showed that the transverse ends of vortex ring, which collided earlier with the wall, induced secondary vortex and entrained it rapidly accompanied with significant reduction of core’s size. This phenomenon is similar to the lower core of vortex ring in oblique collision upon a flat wall. Other part of vortex ring collided with the wall subsequently and induced secondary vortex at different locations and times. Due to the decreasing transverse spacing in the V-shaped groove, azimuthal instabilities developed on primary and secondary vortices. The azimuthal waviness was compressed and displaced toward the longitudinal plane. It was followed by intense self-interaction and three-dimensional vortex stretching between the azimuthal waviness. The entire vortex structure was then stretched longitudinally with the production small scale hairpin vortices. It was found that the greater the vertex angle, the weaker shearing action experienced by the primary vortex. It resulted in stronger induction of boundary layer and secondary vortices which led to more intense interaction between primary and secondary vortex. However, the interaction between boundary layer and small scale hairpin vortices still remain unclear due to its complicated and three-dimensional nature. Future research can be conducted to understand more about the formation and breakdown of small scale vortices at the near-wall region.
author2 New Tze How Daniel
author_facet New Tze How Daniel
Leong, Sheng Yuan
format Final Year Project
author Leong, Sheng Yuan
author_sort Leong, Sheng Yuan
title A numerical simulation study on vortex-ring collisions upon arbitrary solid boundary
title_short A numerical simulation study on vortex-ring collisions upon arbitrary solid boundary
title_full A numerical simulation study on vortex-ring collisions upon arbitrary solid boundary
title_fullStr A numerical simulation study on vortex-ring collisions upon arbitrary solid boundary
title_full_unstemmed A numerical simulation study on vortex-ring collisions upon arbitrary solid boundary
title_sort numerical simulation study on vortex-ring collisions upon arbitrary solid boundary
publishDate 2018
url http://hdl.handle.net/10356/74516
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