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Streamlined bodies drag force estimation using wake integration technique
In this paper, the drag force calculation around the SUBOFF submarine in axisymmetric configuration was investigated using the “Wake Integration Technique.” This method is usually used in wind tunnels as an auxiliary method instead of the common “surface integral technique” for flow around complex g...
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Published in: | Journal of the Brazilian Society of Mechanical Sciences and Engineering 2020-06, Vol.42 (6), Article 293 |
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creator | Talezade Shirazi, Amin Dehghan Manshadi, Mojtaba |
description | In this paper, the drag force calculation around the SUBOFF submarine in axisymmetric configuration was investigated using the “Wake Integration Technique.” This method is usually used in wind tunnels as an auxiliary method instead of the common “surface integral technique” for flow around complex geometries or shock wave flows. The results of this method are dependent on data collection vertex space, distance, and section size, where practical suggestions were made for each parameter in this research. Furthermore, the contribution of the pressure, momentum, and fluctuation terms in the total drag force were also evaluated at different cross sections. These findings can be implemented in wind tunnels with small test section length and also to compare the results obtained by the common surface integral method. Simulations were carried out at different aspect ratios at zero angles of attack, and the capabilities of this method at inclined flows were also discussed. The obtained results were also compared against the common method, and the results show only 4% deviation at zero angle. |
doi_str_mv | 10.1007/s40430-020-02373-8 |
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The results of this method are dependent on data collection vertex space, distance, and section size, where practical suggestions were made for each parameter in this research. Furthermore, the contribution of the pressure, momentum, and fluctuation terms in the total drag force were also evaluated at different cross sections. These findings can be implemented in wind tunnels with small test section length and also to compare the results obtained by the common surface integral method. Simulations were carried out at different aspect ratios at zero angles of attack, and the capabilities of this method at inclined flows were also discussed. The obtained results were also compared against the common method, and the results show only 4% deviation at zero angle.</description><identifier>ISSN: 1678-5878</identifier><identifier>EISSN: 1806-3691</identifier><identifier>DOI: 10.1007/s40430-020-02373-8</identifier><language>eng</language><publisher>Berlin/Heidelberg: Springer Berlin Heidelberg</publisher><subject>Angle of attack ; Aspect ratio ; Drag ; Engineering ; Integrals ; Mechanical Engineering ; Shock waves ; Streamlined bodies ; Technical Paper ; Wind tunnel testing ; Wind tunnels</subject><ispartof>Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2020-06, Vol.42 (6), Article 293</ispartof><rights>The Brazilian Society of Mechanical Sciences and Engineering 2020</rights><rights>The Brazilian Society of Mechanical Sciences and Engineering 2020.</rights><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c319t-a4aad0912a91ffbcce881a8df604b3b3567b8f77ae83bdc4f3fe63de3b8e8df33</citedby><cites>FETCH-LOGICAL-c319t-a4aad0912a91ffbcce881a8df604b3b3567b8f77ae83bdc4f3fe63de3b8e8df33</cites><orcidid>0000-0002-4011-5385</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Talezade Shirazi, Amin</creatorcontrib><creatorcontrib>Dehghan Manshadi, Mojtaba</creatorcontrib><title>Streamlined bodies drag force estimation using wake integration technique</title><title>Journal of the Brazilian Society of Mechanical Sciences and Engineering</title><addtitle>J Braz. 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Simulations were carried out at different aspect ratios at zero angles of attack, and the capabilities of this method at inclined flows were also discussed. The obtained results were also compared against the common method, and the results show only 4% deviation at zero angle.</description><subject>Angle of attack</subject><subject>Aspect ratio</subject><subject>Drag</subject><subject>Engineering</subject><subject>Integrals</subject><subject>Mechanical Engineering</subject><subject>Shock waves</subject><subject>Streamlined bodies</subject><subject>Technical Paper</subject><subject>Wind tunnel testing</subject><subject>Wind tunnels</subject><issn>1678-5878</issn><issn>1806-3691</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><recordid>eNp9kE9LxDAQxYMouK5-AU8Bz9Gk0ybpURb_LCx4UM8hbSa16267JlnEb2_WCt48DDMMvzePeYRcCn4tOFc3seQlcMaLQ4ECpo_ITGguGchaHOdZKs0qrfQpOYtxzTkUlaxmZPmcAtrtph_Q0WZ0PUbqgu2oH0OLFGPqtzb140D3sR86-mnfkfZDwi5M64Tt29B_7PGcnHi7iXjx2-fk9f7uZfHIVk8Py8XtirUg6sRsaa3jtShsLbxv2ha1FlY7L3nZQAOVVI32SlnU0Li29OBRgkNoNGYKYE6upru7MGbbmMx63IchW5qi5KIu6lLyTBUT1YYxxoDe7EL-JHwZwc0hMjNFZnJk5icyo7MIJlHM8NBh-Dv9j-obNEZweA</recordid><startdate>20200601</startdate><enddate>20200601</enddate><creator>Talezade Shirazi, Amin</creator><creator>Dehghan Manshadi, Mojtaba</creator><general>Springer Berlin Heidelberg</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><orcidid>https://orcid.org/0000-0002-4011-5385</orcidid></search><sort><creationdate>20200601</creationdate><title>Streamlined bodies drag force estimation using wake integration technique</title><author>Talezade Shirazi, Amin ; Dehghan Manshadi, Mojtaba</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c319t-a4aad0912a91ffbcce881a8df604b3b3567b8f77ae83bdc4f3fe63de3b8e8df33</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Angle of attack</topic><topic>Aspect ratio</topic><topic>Drag</topic><topic>Engineering</topic><topic>Integrals</topic><topic>Mechanical Engineering</topic><topic>Shock waves</topic><topic>Streamlined bodies</topic><topic>Technical Paper</topic><topic>Wind tunnel testing</topic><topic>Wind tunnels</topic><toplevel>online_resources</toplevel><creatorcontrib>Talezade Shirazi, Amin</creatorcontrib><creatorcontrib>Dehghan Manshadi, Mojtaba</creatorcontrib><collection>CrossRef</collection><jtitle>Journal of the Brazilian Society of Mechanical Sciences and Engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Talezade Shirazi, Amin</au><au>Dehghan Manshadi, Mojtaba</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Streamlined bodies drag force estimation using wake integration technique</atitle><jtitle>Journal of the Brazilian Society of Mechanical Sciences and Engineering</jtitle><stitle>J Braz. 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These findings can be implemented in wind tunnels with small test section length and also to compare the results obtained by the common surface integral method. Simulations were carried out at different aspect ratios at zero angles of attack, and the capabilities of this method at inclined flows were also discussed. The obtained results were also compared against the common method, and the results show only 4% deviation at zero angle.</abstract><cop>Berlin/Heidelberg</cop><pub>Springer Berlin Heidelberg</pub><doi>10.1007/s40430-020-02373-8</doi><orcidid>https://orcid.org/0000-0002-4011-5385</orcidid></addata></record> |
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source | Springer Nature:Jisc Collections:Springer Nature Read and Publish 2023-2025: Springer Reading List |
subjects | Angle of attack Aspect ratio Drag Engineering Integrals Mechanical Engineering Shock waves Streamlined bodies Technical Paper Wind tunnel testing Wind tunnels |
title | Streamlined bodies drag force estimation using wake integration technique |
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