Flow transitions of head-on vortex ring collisions with contaminated air-water interfaces

An experimental study was conducted on head-on collisions of Re = 2000 and 4000 vortex rings upon air-water interfaces to study the vortex dynamics and the effects of different vortex ring Reynolds numbers on the key vortex flow mechanisms. Unfiltered tap water was used where surface contaminants we...

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Main Authors: New, Tze How, Yeo, Kye Wei B., Koh, J. Y., Long, J.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Journal Article
Language:English
Published: 2024
Subjects:
Online Access:https://hdl.handle.net/10356/174717
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author New, Tze How
Yeo, Kye Wei B.
Koh, J. Y.
Long, J.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
New, Tze How
Yeo, Kye Wei B.
Koh, J. Y.
Long, J.
author_sort New, Tze How
collection NTU
description An experimental study was conducted on head-on collisions of Re = 2000 and 4000 vortex rings upon air-water interfaces to study the vortex dynamics and the effects of different vortex ring Reynolds numbers on the key vortex flow mechanisms. Unfiltered tap water was used where surface contaminants were present; hence, the interfacial stress levels are lower but not entirely zero like an idealized free surface. Results demonstrate that the vortex dynamics involve first, the resulting secondary and tertiary vortex rings transitioning into wavy states, before their upper loops disconnect/reconnect to the interface to form U-shaped vortex loops along the inner and outer peripheries of the primary vortex ring, respectively, in an alternating pattern. Second, tertiary vortex loops entangle around the primary vortex ring to produce counter-rotating vortex pairs that reorganize themselves along the primary vortex ring outer periphery, between the primary vortex ring and secondary vortex loops, as well as hairpin-like structures that aid ejection of primary vortex ring momentum. Third, secondary vortex loops rotate toward the collision axis before their lower segments are entrained by the primary vortex ring. A higher Reynolds number primary vortex ring would confer additional flow changes, such as a higher wave number for the secondary and tertiary vortex rings/loops, pairings of secondary vortex loops “side-arms” that reduce their instances by about half and formations of Tsai-Widnall-Moore-Saffman instabilities induced by flow perturbations. Finally, vortex flow models proposed to explain the flow mechanism at different flow stages are found to be in good agreements with the experimental visualizations.
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spelling ntu-10356/1747172024-04-13T16:49:06Z Flow transitions of head-on vortex ring collisions with contaminated air-water interfaces New, Tze How Yeo, Kye Wei B. Koh, J. Y. Long, J. School of Mechanical and Aerospace Engineering Engineering Interface states Air An experimental study was conducted on head-on collisions of Re = 2000 and 4000 vortex rings upon air-water interfaces to study the vortex dynamics and the effects of different vortex ring Reynolds numbers on the key vortex flow mechanisms. Unfiltered tap water was used where surface contaminants were present; hence, the interfacial stress levels are lower but not entirely zero like an idealized free surface. Results demonstrate that the vortex dynamics involve first, the resulting secondary and tertiary vortex rings transitioning into wavy states, before their upper loops disconnect/reconnect to the interface to form U-shaped vortex loops along the inner and outer peripheries of the primary vortex ring, respectively, in an alternating pattern. Second, tertiary vortex loops entangle around the primary vortex ring to produce counter-rotating vortex pairs that reorganize themselves along the primary vortex ring outer periphery, between the primary vortex ring and secondary vortex loops, as well as hairpin-like structures that aid ejection of primary vortex ring momentum. Third, secondary vortex loops rotate toward the collision axis before their lower segments are entrained by the primary vortex ring. A higher Reynolds number primary vortex ring would confer additional flow changes, such as a higher wave number for the secondary and tertiary vortex rings/loops, pairings of secondary vortex loops “side-arms” that reduce their instances by about half and formations of Tsai-Widnall-Moore-Saffman instabilities induced by flow perturbations. Finally, vortex flow models proposed to explain the flow mechanism at different flow stages are found to be in good agreements with the experimental visualizations. Nanyang Technological University The authors acknowledge the support of the present study by CN Yang Scholars Programme and School of Mechanical and Aerospace Engineering, Nanyang Technological University. 2024-04-08T05:45:54Z 2024-04-08T05:45:54Z 2024 Journal Article New, T. H., Yeo, K. W. B., Koh, J. Y. & Long, J. (2024). Flow transitions of head-on vortex ring collisions with contaminated air-water interfaces. Physics of Fluids, 36(1), 014112-. https://dx.doi.org/10.1063/5.0176897 1070-6631 https://hdl.handle.net/10356/174717 10.1063/5.0176897 2-s2.0-85182263017 1 36 014112 en Physics of Fluids © 2024 Author(s). Published under an exclusive license by AIP Publishing. application/pdf
spellingShingle Engineering
Interface states
Air
New, Tze How
Yeo, Kye Wei B.
Koh, J. Y.
Long, J.
Flow transitions of head-on vortex ring collisions with contaminated air-water interfaces
title Flow transitions of head-on vortex ring collisions with contaminated air-water interfaces
title_full Flow transitions of head-on vortex ring collisions with contaminated air-water interfaces
title_fullStr Flow transitions of head-on vortex ring collisions with contaminated air-water interfaces
title_full_unstemmed Flow transitions of head-on vortex ring collisions with contaminated air-water interfaces
title_short Flow transitions of head-on vortex ring collisions with contaminated air-water interfaces
title_sort flow transitions of head on vortex ring collisions with contaminated air water interfaces
topic Engineering
Interface states
Air
url https://hdl.handle.net/10356/174717
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