Effect of variable pitch on flow around a helically twisted elliptic cylinder
We propose a new geometric disturbance called a variable pitch helically twisted elliptical (VPHTE) cylinder that was obtained by combining helically twisted elliptic (HTE) and asymmetric geometries for passive flow control. We confirmed that the new geometric disturbance reduces the drag and lift f...
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description | We propose a new geometric disturbance called a variable pitch helically twisted elliptical (VPHTE) cylinder that was obtained by combining helically twisted elliptic (HTE) and asymmetric geometries for passive flow control. We confirmed that the new geometric disturbance reduces the drag and lift fluctuations compared with the smooth and HTE cylinders at the Reynolds number (Re) of 3000. Large eddy simulation was used for the evaluation of the flow control performance of the VPHTE cylinder at Re = 3000, which corresponds to the subcritical regime. A parametric study was conducted on the variable pitch ratio (VP). The smallest value of the time-averaged drag coefficient of the VPHTE cylinder is lower by about 16.7% and 4.1% than those of the smooth and HTE cylinders, respectively. Furthermore, a VPHTE cylinder reduces the root-mean-square value of the lift coefficient by 96.2% compared with a smooth cylinder. The vortex formation length related to the stabilization of the shear layer of the VPHTE cylinders is longer than those of the smooth and HTE cylinders, and it is consistently elongated as the VP increases. In addition, time-averaged pressure coefficients for different cylinders were compared to analyze the reason for the drag reduction. We systematically investigated the additional flow control performance of the VPHTE cylinders and VP effects by analyzing physical values such as the swirl strength, turbulent kinetic energy, and vorticity components around the VPHTE cylinders. |
doi_str_mv | 10.1063/5.0013735 |
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We confirmed that the new geometric disturbance reduces the drag and lift fluctuations compared with the smooth and HTE cylinders at the Reynolds number (Re) of 3000. Large eddy simulation was used for the evaluation of the flow control performance of the VPHTE cylinder at Re = 3000, which corresponds to the subcritical regime. A parametric study was conducted on the variable pitch ratio (VP). The smallest value of the time-averaged drag coefficient of the VPHTE cylinder is lower by about 16.7% and 4.1% than those of the smooth and HTE cylinders, respectively. Furthermore, a VPHTE cylinder reduces the root-mean-square value of the lift coefficient by 96.2% compared with a smooth cylinder. The vortex formation length related to the stabilization of the shear layer of the VPHTE cylinders is longer than those of the smooth and HTE cylinders, and it is consistently elongated as the VP increases. In addition, time-averaged pressure coefficients for different cylinders were compared to analyze the reason for the drag reduction. We systematically investigated the additional flow control performance of the VPHTE cylinders and VP effects by analyzing physical values such as the swirl strength, turbulent kinetic energy, and vorticity components around the VPHTE cylinders.</description><identifier>ISSN: 2158-3226</identifier><identifier>EISSN: 2158-3226</identifier><identifier>DOI: 10.1063/5.0013735</identifier><identifier>CODEN: AAIDBI</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Aerodynamic coefficients ; Cylinders ; Drag coefficients ; Drag reduction ; Flow control ; Fluid dynamics ; Fluid flow ; Kinetic energy ; Large eddy simulation ; Reynolds number ; Shear layers ; Vorticity</subject><ispartof>AIP advances, 2020-09, Vol.10 (9), p.095215-095215-18</ispartof><rights>Author(s)</rights><rights>2020 Author(s). All article content, except where otherwise noted, is licensed under a Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c393t-dfa70638e460912becdb754be45c886d5dab6882892515c39c675d41834529f23</citedby><cites>FETCH-LOGICAL-c393t-dfa70638e460912becdb754be45c886d5dab6882892515c39c675d41834529f23</cites><orcidid>0000-0001-6082-5715</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,860,2095,27903,27904</link.rule.ids></links><search><creatorcontrib>Moon, Jahoon</creatorcontrib><creatorcontrib>Yoon, Hyun Sik</creatorcontrib><title>Effect of variable pitch on flow around a helically twisted elliptic cylinder</title><title>AIP advances</title><description>We propose a new geometric disturbance called a variable pitch helically twisted elliptical (VPHTE) cylinder that was obtained by combining helically twisted elliptic (HTE) and asymmetric geometries for passive flow control. We confirmed that the new geometric disturbance reduces the drag and lift fluctuations compared with the smooth and HTE cylinders at the Reynolds number (Re) of 3000. Large eddy simulation was used for the evaluation of the flow control performance of the VPHTE cylinder at Re = 3000, which corresponds to the subcritical regime. A parametric study was conducted on the variable pitch ratio (VP). The smallest value of the time-averaged drag coefficient of the VPHTE cylinder is lower by about 16.7% and 4.1% than those of the smooth and HTE cylinders, respectively. Furthermore, a VPHTE cylinder reduces the root-mean-square value of the lift coefficient by 96.2% compared with a smooth cylinder. The vortex formation length related to the stabilization of the shear layer of the VPHTE cylinders is longer than those of the smooth and HTE cylinders, and it is consistently elongated as the VP increases. In addition, time-averaged pressure coefficients for different cylinders were compared to analyze the reason for the drag reduction. We systematically investigated the additional flow control performance of the VPHTE cylinders and VP effects by analyzing physical values such as the swirl strength, turbulent kinetic energy, and vorticity components around the VPHTE cylinders.</description><subject>Aerodynamic coefficients</subject><subject>Cylinders</subject><subject>Drag coefficients</subject><subject>Drag reduction</subject><subject>Flow control</subject><subject>Fluid dynamics</subject><subject>Fluid flow</subject><subject>Kinetic energy</subject><subject>Large eddy simulation</subject><subject>Reynolds number</subject><subject>Shear layers</subject><subject>Vorticity</subject><issn>2158-3226</issn><issn>2158-3226</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><sourceid>DOA</sourceid><recordid>eNp9kE9LAzEQxRdRsNQe_AYBTwpb83c3e5RStVDxoueQnSQ2JW5qNrX027vaIp6cywzDb948XlFcEjwluGK3YooxYTUTJ8WIEiFLRml1-mc-LyZ9v8ZD8YZgyUfF09w5CxlFhz518roNFm18hhWKHXIh7pBOcdsZpNHKBg86hD3KO99na5ANwW-yBwT74Dtj00Vx5nTo7eTYx8Xr_fxl9lgunx8Ws7tlCaxhuTRO14NfaXmFG0JbC6atBW8tFyBlZYTRbSUllQ0VRAw3UNXCcCIZF7RxlI2LxUHXRL1Wm-TfddqrqL36WcT0pnQajAWrCJiGE-DCOsxrwxtMQFaCghEOiIZB6-qgtUnxY2v7rNZxm7rBvqKck4o1kuOBuj5QkGLfJ-t-vxKsvsNXQh3DH9ibA9uDzzr72P0DfwEwq4Gp</recordid><startdate>20200901</startdate><enddate>20200901</enddate><creator>Moon, Jahoon</creator><creator>Yoon, Hyun Sik</creator><general>American Institute of Physics</general><general>AIP Publishing LLC</general><scope>AJDQP</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>DOA</scope><orcidid>https://orcid.org/0000-0001-6082-5715</orcidid></search><sort><creationdate>20200901</creationdate><title>Effect of variable pitch on flow around a helically twisted elliptic cylinder</title><author>Moon, Jahoon ; Yoon, Hyun Sik</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c393t-dfa70638e460912becdb754be45c886d5dab6882892515c39c675d41834529f23</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Aerodynamic coefficients</topic><topic>Cylinders</topic><topic>Drag coefficients</topic><topic>Drag reduction</topic><topic>Flow control</topic><topic>Fluid dynamics</topic><topic>Fluid flow</topic><topic>Kinetic energy</topic><topic>Large eddy simulation</topic><topic>Reynolds number</topic><topic>Shear layers</topic><topic>Vorticity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Moon, Jahoon</creatorcontrib><creatorcontrib>Yoon, Hyun Sik</creatorcontrib><collection>AIP Open Access Journals</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>DOAJ Directory of Open Access Journals</collection><jtitle>AIP advances</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Moon, Jahoon</au><au>Yoon, Hyun Sik</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Effect of variable pitch on flow around a helically twisted elliptic cylinder</atitle><jtitle>AIP advances</jtitle><date>2020-09-01</date><risdate>2020</risdate><volume>10</volume><issue>9</issue><spage>095215</spage><epage>095215-18</epage><pages>095215-095215-18</pages><issn>2158-3226</issn><eissn>2158-3226</eissn><coden>AAIDBI</coden><abstract>We propose a new geometric disturbance called a variable pitch helically twisted elliptical (VPHTE) cylinder that was obtained by combining helically twisted elliptic (HTE) and asymmetric geometries for passive flow control. We confirmed that the new geometric disturbance reduces the drag and lift fluctuations compared with the smooth and HTE cylinders at the Reynolds number (Re) of 3000. Large eddy simulation was used for the evaluation of the flow control performance of the VPHTE cylinder at Re = 3000, which corresponds to the subcritical regime. A parametric study was conducted on the variable pitch ratio (VP). The smallest value of the time-averaged drag coefficient of the VPHTE cylinder is lower by about 16.7% and 4.1% than those of the smooth and HTE cylinders, respectively. Furthermore, a VPHTE cylinder reduces the root-mean-square value of the lift coefficient by 96.2% compared with a smooth cylinder. The vortex formation length related to the stabilization of the shear layer of the VPHTE cylinders is longer than those of the smooth and HTE cylinders, and it is consistently elongated as the VP increases. In addition, time-averaged pressure coefficients for different cylinders were compared to analyze the reason for the drag reduction. We systematically investigated the additional flow control performance of the VPHTE cylinders and VP effects by analyzing physical values such as the swirl strength, turbulent kinetic energy, and vorticity components around the VPHTE cylinders.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/5.0013735</doi><tpages>18</tpages><orcidid>https://orcid.org/0000-0001-6082-5715</orcidid><oa>free_for_read</oa></addata></record> |
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subjects | Aerodynamic coefficients Cylinders Drag coefficients Drag reduction Flow control Fluid dynamics Fluid flow Kinetic energy Large eddy simulation Reynolds number Shear layers Vorticity |
title | Effect of variable pitch on flow around a helically twisted elliptic cylinder |
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