Heat Transfer Enhancement in Narrow Diverging Channels
Detailed heat transfer coefficient distributions have been obtained for narrow diverging channels with and without enhancement features. The cooling configurations considered include rib turbulators and concavities (or dimples) on the main heat transfer surfaces. All of the measurements are presente...
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Veröffentlicht in: | Journal of turbomachinery 2013-07, Vol.135 (4), p.1-7 |
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creator | Lamont, Justin Ramesh, Sridharan Ekkad, Srinath V Tolpadi, Anil Kaminski, Christopher Salamah, Samir |
description | Detailed heat transfer coefficient distributions have been obtained for narrow diverging channels with and without enhancement features. The cooling configurations considered include rib turbulators and concavities (or dimples) on the main heat transfer surfaces. All of the measurements are presented at a representative Reynolds number of 28,000. Pressure drop measurements for the overall channel are also presented to evaluate the heat transfer enhancement geometry with respect to the pumping power requirements. The test models were studied for wall heat transfer coefficient measurements using the transient liquid crystal technique. The model wall inner surfaces were sprayed with thermochromic liquid crystals and a transient test was used to obtain the local heat transfer coefficients from the measured color change. An analysis of the results shows that the choice of designs is limited by the available pressure drop, even if the design provides significantly higher heat transfer coefficients. Dimpled surfaces provide appreciably high heat transfer coefficients and a reasonable pressure drop, whereas ribbed ducts provide significantly higher heat transfer coefficients and a higher overall pressure drop. |
doi_str_mv | 10.1115/1.4007740 |
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The cooling configurations considered include rib turbulators and concavities (or dimples) on the main heat transfer surfaces. All of the measurements are presented at a representative Reynolds number of 28,000. Pressure drop measurements for the overall channel are also presented to evaluate the heat transfer enhancement geometry with respect to the pumping power requirements. The test models were studied for wall heat transfer coefficient measurements using the transient liquid crystal technique. The model wall inner surfaces were sprayed with thermochromic liquid crystals and a transient test was used to obtain the local heat transfer coefficients from the measured color change. An analysis of the results shows that the choice of designs is limited by the available pressure drop, even if the design provides significantly higher heat transfer coefficients. Dimpled surfaces provide appreciably high heat transfer coefficients and a reasonable pressure drop, whereas ribbed ducts provide significantly higher heat transfer coefficients and a higher overall pressure drop.</description><identifier>ISSN: 0889-504X</identifier><identifier>EISSN: 1528-8900</identifier><identifier>DOI: 10.1115/1.4007740</identifier><identifier>CODEN: JOTUEI</identifier><language>eng</language><publisher>New York, NY: ASME</publisher><subject>Analytical and numerical techniques ; Applied sciences ; Channels ; Continuous cycle engines: steam and gas turbines, jet engines ; Design engineering ; Dimpling ; Engines and turbines ; Exact sciences and technology ; Flows in ducts, channels, nozzles, and conduits ; Fluid dynamics ; Fundamental areas of phenomenology (including applications) ; Heat transfer ; Heat transfer coefficients ; Liquid crystals ; Mechanical engineering. Machine design ; Physics ; Pressure drop ; Walls</subject><ispartof>Journal of turbomachinery, 2013-07, Vol.135 (4), p.1-7</ispartof><rights>2014 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a312t-720ccb7b92778cc8e0eaf2a72b31e29cf115e060c3989451d912f83f5b9036563</citedby><cites>FETCH-LOGICAL-a312t-720ccb7b92778cc8e0eaf2a72b31e29cf115e060c3989451d912f83f5b9036563</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925,38520</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=27623741$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Lamont, Justin</creatorcontrib><creatorcontrib>Ramesh, Sridharan</creatorcontrib><creatorcontrib>Ekkad, Srinath V</creatorcontrib><creatorcontrib>Tolpadi, Anil</creatorcontrib><creatorcontrib>Kaminski, Christopher</creatorcontrib><creatorcontrib>Salamah, Samir</creatorcontrib><title>Heat Transfer Enhancement in Narrow Diverging Channels</title><title>Journal of turbomachinery</title><addtitle>J. Turbomach</addtitle><description>Detailed heat transfer coefficient distributions have been obtained for narrow diverging channels with and without enhancement features. The cooling configurations considered include rib turbulators and concavities (or dimples) on the main heat transfer surfaces. All of the measurements are presented at a representative Reynolds number of 28,000. Pressure drop measurements for the overall channel are also presented to evaluate the heat transfer enhancement geometry with respect to the pumping power requirements. The test models were studied for wall heat transfer coefficient measurements using the transient liquid crystal technique. The model wall inner surfaces were sprayed with thermochromic liquid crystals and a transient test was used to obtain the local heat transfer coefficients from the measured color change. An analysis of the results shows that the choice of designs is limited by the available pressure drop, even if the design provides significantly higher heat transfer coefficients. Dimpled surfaces provide appreciably high heat transfer coefficients and a reasonable pressure drop, whereas ribbed ducts provide significantly higher heat transfer coefficients and a higher overall pressure drop.</description><subject>Analytical and numerical techniques</subject><subject>Applied sciences</subject><subject>Channels</subject><subject>Continuous cycle engines: steam and gas turbines, jet engines</subject><subject>Design engineering</subject><subject>Dimpling</subject><subject>Engines and turbines</subject><subject>Exact sciences and technology</subject><subject>Flows in ducts, channels, nozzles, and conduits</subject><subject>Fluid dynamics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Heat transfer</subject><subject>Heat transfer coefficients</subject><subject>Liquid crystals</subject><subject>Mechanical engineering. Machine design</subject><subject>Physics</subject><subject>Pressure drop</subject><subject>Walls</subject><issn>0889-504X</issn><issn>1528-8900</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2013</creationdate><recordtype>article</recordtype><recordid>eNo9kL1PwzAUxC0EEqUwMLNkQYIh5dmOY3tEpXxIFSxFYrMc81xSpU6xUxD_PUatmN5wvzu9O0LOKUwopeKGTioAKSs4ICMqmCqVBjgkI1BKlwKqt2NyktIKgHIuqhGpH9EOxSLakDzGYhY-bHC4xjAUbSiebYz9d3HXfmFctmFZTLMcsEun5MjbLuHZ_o7J6_1sMX0s5y8PT9PbeWk5ZUMpGTjXyEYzKZVzCgGtZ1ayhlNk2vn8MkINjmulK0HfNWVecS8aDbwWNR-Tq13uJvafW0yDWbfJYdfZgP02mVwRNOfZnNHrHepin1JEbzaxXdv4YyiYv20MNfttMnu5j7XJ2c7n-q5N_wYma8ZlRTN3seNsWqNZ9dsYclvDpaIg-C-XbWnU</recordid><startdate>20130701</startdate><enddate>20130701</enddate><creator>Lamont, Justin</creator><creator>Ramesh, Sridharan</creator><creator>Ekkad, Srinath V</creator><creator>Tolpadi, Anil</creator><creator>Kaminski, Christopher</creator><creator>Salamah, Samir</creator><general>ASME</general><general>American Society of Mechanical Engineers</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20130701</creationdate><title>Heat Transfer Enhancement in Narrow Diverging Channels</title><author>Lamont, Justin ; Ramesh, Sridharan ; Ekkad, Srinath V ; Tolpadi, Anil ; Kaminski, Christopher ; Salamah, Samir</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a312t-720ccb7b92778cc8e0eaf2a72b31e29cf115e060c3989451d912f83f5b9036563</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2013</creationdate><topic>Analytical and numerical techniques</topic><topic>Applied sciences</topic><topic>Channels</topic><topic>Continuous cycle engines: steam and gas turbines, jet engines</topic><topic>Design engineering</topic><topic>Dimpling</topic><topic>Engines and turbines</topic><topic>Exact sciences and technology</topic><topic>Flows in ducts, channels, nozzles, and conduits</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Heat transfer</topic><topic>Heat transfer coefficients</topic><topic>Liquid crystals</topic><topic>Mechanical engineering. Machine design</topic><topic>Physics</topic><topic>Pressure drop</topic><topic>Walls</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Lamont, Justin</creatorcontrib><creatorcontrib>Ramesh, Sridharan</creatorcontrib><creatorcontrib>Ekkad, Srinath V</creatorcontrib><creatorcontrib>Tolpadi, Anil</creatorcontrib><creatorcontrib>Kaminski, Christopher</creatorcontrib><creatorcontrib>Salamah, Samir</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of turbomachinery</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Lamont, Justin</au><au>Ramesh, Sridharan</au><au>Ekkad, Srinath V</au><au>Tolpadi, Anil</au><au>Kaminski, Christopher</au><au>Salamah, Samir</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Heat Transfer Enhancement in Narrow Diverging Channels</atitle><jtitle>Journal of turbomachinery</jtitle><stitle>J. Turbomach</stitle><date>2013-07-01</date><risdate>2013</risdate><volume>135</volume><issue>4</issue><spage>1</spage><epage>7</epage><pages>1-7</pages><issn>0889-504X</issn><eissn>1528-8900</eissn><coden>JOTUEI</coden><abstract>Detailed heat transfer coefficient distributions have been obtained for narrow diverging channels with and without enhancement features. The cooling configurations considered include rib turbulators and concavities (or dimples) on the main heat transfer surfaces. All of the measurements are presented at a representative Reynolds number of 28,000. Pressure drop measurements for the overall channel are also presented to evaluate the heat transfer enhancement geometry with respect to the pumping power requirements. The test models were studied for wall heat transfer coefficient measurements using the transient liquid crystal technique. The model wall inner surfaces were sprayed with thermochromic liquid crystals and a transient test was used to obtain the local heat transfer coefficients from the measured color change. An analysis of the results shows that the choice of designs is limited by the available pressure drop, even if the design provides significantly higher heat transfer coefficients. Dimpled surfaces provide appreciably high heat transfer coefficients and a reasonable pressure drop, whereas ribbed ducts provide significantly higher heat transfer coefficients and a higher overall pressure drop.</abstract><cop>New York, NY</cop><pub>ASME</pub><doi>10.1115/1.4007740</doi><tpages>7</tpages></addata></record> |
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source | ASME Transactions Journals (Current); Alma/SFX Local Collection |
subjects | Analytical and numerical techniques Applied sciences Channels Continuous cycle engines: steam and gas turbines, jet engines Design engineering Dimpling Engines and turbines Exact sciences and technology Flows in ducts, channels, nozzles, and conduits Fluid dynamics Fundamental areas of phenomenology (including applications) Heat transfer Heat transfer coefficients Liquid crystals Mechanical engineering. Machine design Physics Pressure drop Walls |
title | Heat Transfer Enhancement in Narrow Diverging Channels |
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