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Numerical study on the aerodynamic characteristics and flow field of two tandem tapered square cylinders with different spacing ratios
Three-dimensional (3-D) large eddy simulations (LES) are carried out to explore the influence of spacing ratio G/D on the flow structures and aerodynamic interference mechanism of two tandem square cylinders with and without tapered modification (taper ratio ξ = 0 % and 5 %) at Reynolds number Re = ...
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Published in: | Ocean engineering 2024-03, Vol.295, p.116875, Article 116875 |
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description | Three-dimensional (3-D) large eddy simulations (LES) are carried out to explore the influence of spacing ratio G/D on the flow structures and aerodynamic interference mechanism of two tandem square cylinders with and without tapered modification (taper ratio ξ = 0 % and 5 %) at Reynolds number Re = 2 × 103. Different spacing ratios G/D from 1.4 to 6.0 are considered, where G is the cylinder center-to-center distance and D is the cylinder width. The flow structures, wind pressure distributions, force coefficients, and power spectral density of the two cylinders are comprehensively analyzed and discussed. The mathematical relationship between spacing ratio and force coefficients is established, which can provide theoretical reference for the design and construction of tandem structures. The results indicate that the flow structures and aerodynamic forces are very sensitive to the spacing and taper ratios. The flow structures of the two cylinders can be divided into three flow regimes based on G/D: single body, reattachment, and co-shedding regimes. As the taper ratio increases, the cross-sectional width of the two cylinders gradually narrows along the height, which in turn weakens the interference effect between the two cylinders and decreases the range of the critical spacing ratio. The width of the shear layer becomes gradually narrower and closer to the surfaces of the two cylinders, resulting in a higher frequency and lower energy of vortex shedding. In addition, the mean and fluctuating wind pressure coefficients, the mean force coefficients in the along-wind direction, and the fluctuating coefficients all decrease with the increase in taper ratio, which is attributed to the reduction of the periodicity and consistency of vortex shedding. Meanwhile, there are weaker mean and fluctuating wind pressure and force coefficients for the two cylinders under the reattachment flow regime. Therefore, in the design and construction of tandem structures for ocean engineering, it should be considered to improve the wind resistance performance by making the structures in the reattachment flow regime.
•The influence of spacing ratios of G/D = 1.4, 2, 3, 4, 4.5, 5, 5.2, 5.4, and 6 on the mean force coefficient, fluctuating force coefficient, vortex shedding frequency, mean wind pressure, and fluctuating wind pressure of the two tandem square cylinders with taper ratios ξ = 0 % and 5 % are comprehensively studied based on the LES approach.•The mechanism of variation in |
doi_str_mv | 10.1016/j.oceaneng.2024.116875 |
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•The influence of spacing ratios of G/D = 1.4, 2, 3, 4, 4.5, 5, 5.2, 5.4, and 6 on the mean force coefficient, fluctuating force coefficient, vortex shedding frequency, mean wind pressure, and fluctuating wind pressure of the two tandem square cylinders with taper ratios ξ = 0 % and 5 % are comprehensively studied based on the LES approach.•The mechanism of variation in the aerodynamic characteristics is revealed via the flow field and 3D vortex structures.•The mathematical relationship between the spacing ratio and the aerodynamic characteristics is established.•A spacing ratio (reattachment flow regime) was recommended to improve the wind resistance performance of the tandem structures in ocean engineering.</description><identifier>ISSN: 0029-8018</identifier><identifier>EISSN: 1873-5258</identifier><identifier>DOI: 10.1016/j.oceaneng.2024.116875</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Aerodynamic characteristics ; Flow field ; LES approach ; Spacing ratios ; Tapered modification ; Two tandem square cylinders</subject><ispartof>Ocean engineering, 2024-03, Vol.295, p.116875, Article 116875</ispartof><rights>2024 Elsevier Ltd</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c312t-8d6940b6ea75c9fe29b6558844f337568614ece2268c585ea09bd6523c23fd713</citedby><cites>FETCH-LOGICAL-c312t-8d6940b6ea75c9fe29b6558844f337568614ece2268c585ea09bd6523c23fd713</cites><orcidid>0000-0001-9338-7555</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27903,27904</link.rule.ids></links><search><creatorcontrib>Jing, Hongmiao</creatorcontrib><creatorcontrib>Zhang, Jitao</creatorcontrib><creatorcontrib>Han, Mengjiao</creatorcontrib><creatorcontrib>Li, Weikang</creatorcontrib><creatorcontrib>Zhao, Wanru</creatorcontrib><creatorcontrib>Liu, Qingkuan</creatorcontrib><title>Numerical study on the aerodynamic characteristics and flow field of two tandem tapered square cylinders with different spacing ratios</title><title>Ocean engineering</title><description>Three-dimensional (3-D) large eddy simulations (LES) are carried out to explore the influence of spacing ratio G/D on the flow structures and aerodynamic interference mechanism of two tandem square cylinders with and without tapered modification (taper ratio ξ = 0 % and 5 %) at Reynolds number Re = 2 × 103. Different spacing ratios G/D from 1.4 to 6.0 are considered, where G is the cylinder center-to-center distance and D is the cylinder width. The flow structures, wind pressure distributions, force coefficients, and power spectral density of the two cylinders are comprehensively analyzed and discussed. The mathematical relationship between spacing ratio and force coefficients is established, which can provide theoretical reference for the design and construction of tandem structures. The results indicate that the flow structures and aerodynamic forces are very sensitive to the spacing and taper ratios. The flow structures of the two cylinders can be divided into three flow regimes based on G/D: single body, reattachment, and co-shedding regimes. As the taper ratio increases, the cross-sectional width of the two cylinders gradually narrows along the height, which in turn weakens the interference effect between the two cylinders and decreases the range of the critical spacing ratio. The width of the shear layer becomes gradually narrower and closer to the surfaces of the two cylinders, resulting in a higher frequency and lower energy of vortex shedding. In addition, the mean and fluctuating wind pressure coefficients, the mean force coefficients in the along-wind direction, and the fluctuating coefficients all decrease with the increase in taper ratio, which is attributed to the reduction of the periodicity and consistency of vortex shedding. Meanwhile, there are weaker mean and fluctuating wind pressure and force coefficients for the two cylinders under the reattachment flow regime. Therefore, in the design and construction of tandem structures for ocean engineering, it should be considered to improve the wind resistance performance by making the structures in the reattachment flow regime.
•The influence of spacing ratios of G/D = 1.4, 2, 3, 4, 4.5, 5, 5.2, 5.4, and 6 on the mean force coefficient, fluctuating force coefficient, vortex shedding frequency, mean wind pressure, and fluctuating wind pressure of the two tandem square cylinders with taper ratios ξ = 0 % and 5 % are comprehensively studied based on the LES approach.•The mechanism of variation in the aerodynamic characteristics is revealed via the flow field and 3D vortex structures.•The mathematical relationship between the spacing ratio and the aerodynamic characteristics is established.•A spacing ratio (reattachment flow regime) was recommended to improve the wind resistance performance of the tandem structures in ocean engineering.</description><subject>Aerodynamic characteristics</subject><subject>Flow field</subject><subject>LES approach</subject><subject>Spacing ratios</subject><subject>Tapered modification</subject><subject>Two tandem square cylinders</subject><issn>0029-8018</issn><issn>1873-5258</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><recordid>eNqFkM1u2zAQhIkgBeqkfYViX0AOSYkUdUsRND9A0FzSM0EvlzENWXRIOoZfoM8dBW7OPQ0wOzNYfIz9EHwpuNBXm2VCchNNL0vJZbcUQptenbGFMH3bKKnMOVtwLofGcGG-sotSNpxzrXm7YH9_77eUI7oRSt37I6QJ6prAUU7-OLltRMC1yw7rHCs1YgE3eQhjOkCINHpIAeohQZ1t2s6yo0weyuveZQI8jnH2c4FDrGvwMYT5PFUoO4dxeoHsakzlG_sS3Fjo-z-9ZH9ufz3f3DePT3cPNz8fG2yFrI3xeuj4SpPrFQ6B5LDSShnTdaFte6WNFh0hSakNKqPI8WHltZItyjb4XrSXTJ92MadSMgW7y3Hr8tEKbj9o2o39pGk_aNoTzbl4fSrS_N1bpGwLRpqQfMyE1foU_zfxDivfhG0</recordid><startdate>20240301</startdate><enddate>20240301</enddate><creator>Jing, Hongmiao</creator><creator>Zhang, Jitao</creator><creator>Han, Mengjiao</creator><creator>Li, Weikang</creator><creator>Zhao, Wanru</creator><creator>Liu, Qingkuan</creator><general>Elsevier Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><orcidid>https://orcid.org/0000-0001-9338-7555</orcidid></search><sort><creationdate>20240301</creationdate><title>Numerical study on the aerodynamic characteristics and flow field of two tandem tapered square cylinders with different spacing ratios</title><author>Jing, Hongmiao ; Zhang, Jitao ; Han, Mengjiao ; Li, Weikang ; Zhao, Wanru ; Liu, Qingkuan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c312t-8d6940b6ea75c9fe29b6558844f337568614ece2268c585ea09bd6523c23fd713</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Aerodynamic characteristics</topic><topic>Flow field</topic><topic>LES approach</topic><topic>Spacing ratios</topic><topic>Tapered modification</topic><topic>Two tandem square cylinders</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Jing, Hongmiao</creatorcontrib><creatorcontrib>Zhang, Jitao</creatorcontrib><creatorcontrib>Han, Mengjiao</creatorcontrib><creatorcontrib>Li, Weikang</creatorcontrib><creatorcontrib>Zhao, Wanru</creatorcontrib><creatorcontrib>Liu, Qingkuan</creatorcontrib><collection>CrossRef</collection><jtitle>Ocean engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Jing, Hongmiao</au><au>Zhang, Jitao</au><au>Han, Mengjiao</au><au>Li, Weikang</au><au>Zhao, Wanru</au><au>Liu, Qingkuan</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Numerical study on the aerodynamic characteristics and flow field of two tandem tapered square cylinders with different spacing ratios</atitle><jtitle>Ocean engineering</jtitle><date>2024-03-01</date><risdate>2024</risdate><volume>295</volume><spage>116875</spage><pages>116875-</pages><artnum>116875</artnum><issn>0029-8018</issn><eissn>1873-5258</eissn><abstract>Three-dimensional (3-D) large eddy simulations (LES) are carried out to explore the influence of spacing ratio G/D on the flow structures and aerodynamic interference mechanism of two tandem square cylinders with and without tapered modification (taper ratio ξ = 0 % and 5 %) at Reynolds number Re = 2 × 103. Different spacing ratios G/D from 1.4 to 6.0 are considered, where G is the cylinder center-to-center distance and D is the cylinder width. The flow structures, wind pressure distributions, force coefficients, and power spectral density of the two cylinders are comprehensively analyzed and discussed. The mathematical relationship between spacing ratio and force coefficients is established, which can provide theoretical reference for the design and construction of tandem structures. The results indicate that the flow structures and aerodynamic forces are very sensitive to the spacing and taper ratios. The flow structures of the two cylinders can be divided into three flow regimes based on G/D: single body, reattachment, and co-shedding regimes. As the taper ratio increases, the cross-sectional width of the two cylinders gradually narrows along the height, which in turn weakens the interference effect between the two cylinders and decreases the range of the critical spacing ratio. The width of the shear layer becomes gradually narrower and closer to the surfaces of the two cylinders, resulting in a higher frequency and lower energy of vortex shedding. In addition, the mean and fluctuating wind pressure coefficients, the mean force coefficients in the along-wind direction, and the fluctuating coefficients all decrease with the increase in taper ratio, which is attributed to the reduction of the periodicity and consistency of vortex shedding. Meanwhile, there are weaker mean and fluctuating wind pressure and force coefficients for the two cylinders under the reattachment flow regime. Therefore, in the design and construction of tandem structures for ocean engineering, it should be considered to improve the wind resistance performance by making the structures in the reattachment flow regime.
•The influence of spacing ratios of G/D = 1.4, 2, 3, 4, 4.5, 5, 5.2, 5.4, and 6 on the mean force coefficient, fluctuating force coefficient, vortex shedding frequency, mean wind pressure, and fluctuating wind pressure of the two tandem square cylinders with taper ratios ξ = 0 % and 5 % are comprehensively studied based on the LES approach.•The mechanism of variation in the aerodynamic characteristics is revealed via the flow field and 3D vortex structures.•The mathematical relationship between the spacing ratio and the aerodynamic characteristics is established.•A spacing ratio (reattachment flow regime) was recommended to improve the wind resistance performance of the tandem structures in ocean engineering.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.oceaneng.2024.116875</doi><orcidid>https://orcid.org/0000-0001-9338-7555</orcidid></addata></record> |
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subjects | Aerodynamic characteristics Flow field LES approach Spacing ratios Tapered modification Two tandem square cylinders |
title | Numerical study on the aerodynamic characteristics and flow field of two tandem tapered square cylinders with different spacing ratios |
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