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Effect of wall proximity in fluid flow and heat transfer from a rectangular prism placed inside a wind tunnel
Experimental investigations in fluid flow and heat transfer have been carried out to study the effect of wall proximity due to flow separation around rectangular prisms. Experiments have been carried out for the Reynolds number 4.9 × 10 4, blockage ratios are 0.1, 0.2, 0.3 and 0.4, aspect ratio ( d...
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Published in: | International journal of heat and mass transfer 2008-02, Vol.51 (3), p.736-746 |
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description | Experimental investigations in fluid flow and heat transfer have been carried out to study the effect of wall proximity due to flow separation around rectangular prisms. Experiments have been carried out for the Reynolds number 4.9
×
10
4, blockage ratios are 0.1, 0.2, 0.3 and 0.4, aspect ratio
(
d
/
c
)
are 1.5, 1.33, 0.667 and 0.333, different height-ratios and various angles of attack. The static pressure distribution has been measured on all faces of the rectangular prisms. The results have been presented in the form of pressure coefficient, drag coefficient for various height-ratios and blockage ratios. The pressure distribution shows positive values on the front face whereas on the rear face negative values of the pressure coefficient have been observed. The positive pressure coefficient for different height-ratios does not vary too much but the negative values of pressure coefficient are higher for all points on the surface as the bluff body approaches the upper wall of the wind tunnel. The drag coefficient decreases with the increase in angle of attack as the height-ratio decreases. There is no definite angle of attack for all blockage ratios and Reynolds numbers at which the value of drag coefficient is either maximum or minimum. The heat transfer experiments have been carried out under constant heat flux condition. Heat transfer coefficient are determined from the measured wall temperature and ambient temperature and presented in the form of Nusselt number. Both local and average Nusselt numbers have been presented for various height-ratios. The variation of local Nusselt number has been shown with non-dimensional distance for different angles of attack and blockage ratios. The variation of average Nusselt number has also been shown with different angles of attack for blockage ratios. The local as well as average Nusselt number decreases as the height-ratio decreases for all non-dimensional distance and angle of attack, respectively, for rectangular prisms. The average Nusselt number for rectangular prisms of different blockage ratio varies with the angle of attack. But there is no definite angle of attack at different blockage ratio at which the value of average Nusselt number is either maximum or minimum. Empirical correlations for average Nusselt number have been presented for rectangular prism as a function of Reynolds number, Prandtl number and relevant non-dimensional parameters. |
doi_str_mv | 10.1016/j.ijheatmasstransfer.2007.04.039 |
format | article |
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×
10
4, blockage ratios are 0.1, 0.2, 0.3 and 0.4, aspect ratio
(
d
/
c
)
are 1.5, 1.33, 0.667 and 0.333, different height-ratios and various angles of attack. The static pressure distribution has been measured on all faces of the rectangular prisms. The results have been presented in the form of pressure coefficient, drag coefficient for various height-ratios and blockage ratios. The pressure distribution shows positive values on the front face whereas on the rear face negative values of the pressure coefficient have been observed. The positive pressure coefficient for different height-ratios does not vary too much but the negative values of pressure coefficient are higher for all points on the surface as the bluff body approaches the upper wall of the wind tunnel. The drag coefficient decreases with the increase in angle of attack as the height-ratio decreases. There is no definite angle of attack for all blockage ratios and Reynolds numbers at which the value of drag coefficient is either maximum or minimum. The heat transfer experiments have been carried out under constant heat flux condition. Heat transfer coefficient are determined from the measured wall temperature and ambient temperature and presented in the form of Nusselt number. Both local and average Nusselt numbers have been presented for various height-ratios. The variation of local Nusselt number has been shown with non-dimensional distance for different angles of attack and blockage ratios. The variation of average Nusselt number has also been shown with different angles of attack for blockage ratios. The local as well as average Nusselt number decreases as the height-ratio decreases for all non-dimensional distance and angle of attack, respectively, for rectangular prisms. The average Nusselt number for rectangular prisms of different blockage ratio varies with the angle of attack. But there is no definite angle of attack at different blockage ratio at which the value of average Nusselt number is either maximum or minimum. Empirical correlations for average Nusselt number have been presented for rectangular prism as a function of Reynolds number, Prandtl number and relevant non-dimensional parameters.</description><identifier>ISSN: 0017-9310</identifier><identifier>EISSN: 1879-2189</identifier><identifier>DOI: 10.1016/j.ijheatmasstransfer.2007.04.039</identifier><identifier>CODEN: IJHMAK</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>Angle of attack ; Applied sciences ; Blockage ratio ; Drag coefficient ; Energy ; Energy. Thermal use of fuels ; Exact sciences and technology ; Flow separation ; Fluid dynamics ; Fundamental areas of phenomenology (including applications) ; Heat transfer ; Height-ratio ; Instrumentation for fluid dynamics ; Nusselt number ; Physics ; Pressure coefficient ; Rectangular prism ; Rotational flow and vorticity ; Separated flows ; Theoretical studies. Data and constants. Metering</subject><ispartof>International journal of heat and mass transfer, 2008-02, Vol.51 (3), p.736-746</ispartof><rights>2007 Elsevier Ltd</rights><rights>2008 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c403t-e743a48cd21e1a9835c3ed0a902f7e4c0f5550e7e4266624a8af4a225fe341953</citedby><cites>FETCH-LOGICAL-c403t-e743a48cd21e1a9835c3ed0a902f7e4c0f5550e7e4266624a8af4a225fe341953</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27923,27924</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=20037739$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Chakrabarty, Dipes</creatorcontrib><creatorcontrib>Brahma, Ranajit Kumar</creatorcontrib><title>Effect of wall proximity in fluid flow and heat transfer from a rectangular prism placed inside a wind tunnel</title><title>International journal of heat and mass transfer</title><description>Experimental investigations in fluid flow and heat transfer have been carried out to study the effect of wall proximity due to flow separation around rectangular prisms. Experiments have been carried out for the Reynolds number 4.9
×
10
4, blockage ratios are 0.1, 0.2, 0.3 and 0.4, aspect ratio
(
d
/
c
)
are 1.5, 1.33, 0.667 and 0.333, different height-ratios and various angles of attack. The static pressure distribution has been measured on all faces of the rectangular prisms. The results have been presented in the form of pressure coefficient, drag coefficient for various height-ratios and blockage ratios. The pressure distribution shows positive values on the front face whereas on the rear face negative values of the pressure coefficient have been observed. The positive pressure coefficient for different height-ratios does not vary too much but the negative values of pressure coefficient are higher for all points on the surface as the bluff body approaches the upper wall of the wind tunnel. The drag coefficient decreases with the increase in angle of attack as the height-ratio decreases. There is no definite angle of attack for all blockage ratios and Reynolds numbers at which the value of drag coefficient is either maximum or minimum. The heat transfer experiments have been carried out under constant heat flux condition. Heat transfer coefficient are determined from the measured wall temperature and ambient temperature and presented in the form of Nusselt number. Both local and average Nusselt numbers have been presented for various height-ratios. The variation of local Nusselt number has been shown with non-dimensional distance for different angles of attack and blockage ratios. The variation of average Nusselt number has also been shown with different angles of attack for blockage ratios. The local as well as average Nusselt number decreases as the height-ratio decreases for all non-dimensional distance and angle of attack, respectively, for rectangular prisms. The average Nusselt number for rectangular prisms of different blockage ratio varies with the angle of attack. But there is no definite angle of attack at different blockage ratio at which the value of average Nusselt number is either maximum or minimum. Empirical correlations for average Nusselt number have been presented for rectangular prism as a function of Reynolds number, Prandtl number and relevant non-dimensional parameters.</description><subject>Angle of attack</subject><subject>Applied sciences</subject><subject>Blockage ratio</subject><subject>Drag coefficient</subject><subject>Energy</subject><subject>Energy. Thermal use of fuels</subject><subject>Exact sciences and technology</subject><subject>Flow separation</subject><subject>Fluid dynamics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Heat transfer</subject><subject>Height-ratio</subject><subject>Instrumentation for fluid dynamics</subject><subject>Nusselt number</subject><subject>Physics</subject><subject>Pressure coefficient</subject><subject>Rectangular prism</subject><subject>Rotational flow and vorticity</subject><subject>Separated flows</subject><subject>Theoretical studies. Data and constants. Metering</subject><issn>0017-9310</issn><issn>1879-2189</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2008</creationdate><recordtype>article</recordtype><recordid>eNqNkEtP3TAUhC3UStzS_gdvQN0kHD_y2lEh2oKQ2NC1deQcF185CdhJL_ff1-HSbtiw8UP6ZkYzjH0VUAoQ9fm29NsHwnnAlOaIY3IUSwnQlKBLUN0R24i26Qop2u4D2wCIpuiUgGP2KaXt-gVdb9hw5RzZmU-O7zAE_hinZz_4ec_9yF1YfJ_Pacdx7Pkax_9lcRengSOPWY3j7yVgzGKfBv4Y0FKf9cn3lImdz9p5GUcKn9lHhyHRl9f7hP36fnV_-bO4vftxffnttrAa1FxQoxXq1vZSkMCuVZVV1AN2IF1D2oKrqgooP2Vd11Jji06jlJUjpUVXqRN2dvDNdZ4WSrMZfLIUAo40Lcko0eiukit4cQBtnFKK5EzuMGDcGwFm3dlszdudzbqzAW3yztni9DULk8XgMmN9-u-TUdU0L9zNgaNc_I_PLsl6GvNUft3Q9JN_f-hfyBuhYg</recordid><startdate>20080201</startdate><enddate>20080201</enddate><creator>Chakrabarty, Dipes</creator><creator>Brahma, Ranajit Kumar</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>KR7</scope><scope>L7M</scope></search><sort><creationdate>20080201</creationdate><title>Effect of wall proximity in fluid flow and heat transfer from a rectangular prism placed inside a wind tunnel</title><author>Chakrabarty, Dipes ; Brahma, Ranajit Kumar</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c403t-e743a48cd21e1a9835c3ed0a902f7e4c0f5550e7e4266624a8af4a225fe341953</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2008</creationdate><topic>Angle of attack</topic><topic>Applied sciences</topic><topic>Blockage ratio</topic><topic>Drag coefficient</topic><topic>Energy</topic><topic>Energy. Thermal use of fuels</topic><topic>Exact sciences and technology</topic><topic>Flow separation</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Heat transfer</topic><topic>Height-ratio</topic><topic>Instrumentation for fluid dynamics</topic><topic>Nusselt number</topic><topic>Physics</topic><topic>Pressure coefficient</topic><topic>Rectangular prism</topic><topic>Rotational flow and vorticity</topic><topic>Separated flows</topic><topic>Theoretical studies. Data and constants. Metering</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chakrabarty, Dipes</creatorcontrib><creatorcontrib>Brahma, Ranajit Kumar</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>International journal of heat and mass transfer</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Chakrabarty, Dipes</au><au>Brahma, Ranajit Kumar</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Effect of wall proximity in fluid flow and heat transfer from a rectangular prism placed inside a wind tunnel</atitle><jtitle>International journal of heat and mass transfer</jtitle><date>2008-02-01</date><risdate>2008</risdate><volume>51</volume><issue>3</issue><spage>736</spage><epage>746</epage><pages>736-746</pages><issn>0017-9310</issn><eissn>1879-2189</eissn><coden>IJHMAK</coden><abstract>Experimental investigations in fluid flow and heat transfer have been carried out to study the effect of wall proximity due to flow separation around rectangular prisms. Experiments have been carried out for the Reynolds number 4.9
×
10
4, blockage ratios are 0.1, 0.2, 0.3 and 0.4, aspect ratio
(
d
/
c
)
are 1.5, 1.33, 0.667 and 0.333, different height-ratios and various angles of attack. The static pressure distribution has been measured on all faces of the rectangular prisms. The results have been presented in the form of pressure coefficient, drag coefficient for various height-ratios and blockage ratios. The pressure distribution shows positive values on the front face whereas on the rear face negative values of the pressure coefficient have been observed. The positive pressure coefficient for different height-ratios does not vary too much but the negative values of pressure coefficient are higher for all points on the surface as the bluff body approaches the upper wall of the wind tunnel. The drag coefficient decreases with the increase in angle of attack as the height-ratio decreases. There is no definite angle of attack for all blockage ratios and Reynolds numbers at which the value of drag coefficient is either maximum or minimum. The heat transfer experiments have been carried out under constant heat flux condition. Heat transfer coefficient are determined from the measured wall temperature and ambient temperature and presented in the form of Nusselt number. Both local and average Nusselt numbers have been presented for various height-ratios. The variation of local Nusselt number has been shown with non-dimensional distance for different angles of attack and blockage ratios. The variation of average Nusselt number has also been shown with different angles of attack for blockage ratios. The local as well as average Nusselt number decreases as the height-ratio decreases for all non-dimensional distance and angle of attack, respectively, for rectangular prisms. The average Nusselt number for rectangular prisms of different blockage ratio varies with the angle of attack. But there is no definite angle of attack at different blockage ratio at which the value of average Nusselt number is either maximum or minimum. Empirical correlations for average Nusselt number have been presented for rectangular prism as a function of Reynolds number, Prandtl number and relevant non-dimensional parameters.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.ijheatmasstransfer.2007.04.039</doi><tpages>11</tpages></addata></record> |
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source | ScienceDirect Journals |
subjects | Angle of attack Applied sciences Blockage ratio Drag coefficient Energy Energy. Thermal use of fuels Exact sciences and technology Flow separation Fluid dynamics Fundamental areas of phenomenology (including applications) Heat transfer Height-ratio Instrumentation for fluid dynamics Nusselt number Physics Pressure coefficient Rectangular prism Rotational flow and vorticity Separated flows Theoretical studies. Data and constants. Metering |
title | Effect of wall proximity in fluid flow and heat transfer from a rectangular prism placed inside a wind tunnel |
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