Loading…

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...

Full description

Saved in:
Bibliographic Details
Published in:International journal of heat and mass transfer 2008-02, Vol.51 (3), p.736-746
Main Authors: Chakrabarty, Dipes, Brahma, Ranajit Kumar
Format: Article
Language:English
Subjects:
Citations: Items that this one cites
Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by cdi_FETCH-LOGICAL-c403t-e743a48cd21e1a9835c3ed0a902f7e4c0f5550e7e4266624a8af4a225fe341953
cites cdi_FETCH-LOGICAL-c403t-e743a48cd21e1a9835c3ed0a902f7e4c0f5550e7e4266624a8af4a225fe341953
container_end_page 746
container_issue 3
container_start_page 736
container_title International journal of heat and mass transfer
container_volume 51
creator Chakrabarty, Dipes
Brahma, Ranajit Kumar
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
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_31749525</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0017931007003559</els_id><sourcerecordid>31749525</sourcerecordid><originalsourceid>FETCH-LOGICAL-c403t-e743a48cd21e1a9835c3ed0a902f7e4c0f5550e7e4266624a8af4a225fe341953</originalsourceid><addsrcrecordid>eNqNkEtP3TAUhC3UStzS_gdvQN0kHD_y2lEh2oKQ2NC1deQcF185CdhJL_ff1-HSbtiw8UP6ZkYzjH0VUAoQ9fm29NsHwnnAlOaIY3IUSwnQlKBLUN0R24i26Qop2u4D2wCIpuiUgGP2KaXt-gVdb9hw5RzZmU-O7zAE_hinZz_4ec_9yF1YfJ_Pacdx7Pkax_9lcRengSOPWY3j7yVgzGKfBv4Y0FKf9cn3lImdz9p5GUcKn9lHhyHRl9f7hP36fnV_-bO4vftxffnttrAa1FxQoxXq1vZSkMCuVZVV1AN2IF1D2oKrqgooP2Vd11Jji06jlJUjpUVXqRN2dvDNdZ4WSrMZfLIUAo40Lcko0eiukit4cQBtnFKK5EzuMGDcGwFm3dlszdudzbqzAW3yztni9DULk8XgMmN9-u-TUdU0L9zNgaNc_I_PLsl6GvNUft3Q9JN_f-hfyBuhYg</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>31749525</pqid></control><display><type>article</type><title>Effect of wall proximity in fluid flow and heat transfer from a rectangular prism placed inside a wind tunnel</title><source>ScienceDirect Journals</source><creator>Chakrabarty, Dipes ; Brahma, Ranajit Kumar</creator><creatorcontrib>Chakrabarty, Dipes ; Brahma, Ranajit Kumar</creatorcontrib><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><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&amp;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 &amp; 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>
fulltext fulltext
identifier ISSN: 0017-9310
ispartof International journal of heat and mass transfer, 2008-02, Vol.51 (3), p.736-746
issn 0017-9310
1879-2189
language eng
recordid cdi_proquest_miscellaneous_31749525
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
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-09T04%3A06%3A57IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Effect%20of%20wall%20proximity%20in%20fluid%20flow%20and%20heat%20transfer%20from%20a%20rectangular%20prism%20placed%20inside%20a%20wind%20tunnel&rft.jtitle=International%20journal%20of%20heat%20and%20mass%20transfer&rft.au=Chakrabarty,%20Dipes&rft.date=2008-02-01&rft.volume=51&rft.issue=3&rft.spage=736&rft.epage=746&rft.pages=736-746&rft.issn=0017-9310&rft.eissn=1879-2189&rft.coden=IJHMAK&rft_id=info:doi/10.1016/j.ijheatmasstransfer.2007.04.039&rft_dat=%3Cproquest_cross%3E31749525%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c403t-e743a48cd21e1a9835c3ed0a902f7e4c0f5550e7e4266624a8af4a225fe341953%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=31749525&rft_id=info:pmid/&rfr_iscdi=true