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Effect of jet direction on heat/mass transfer of rotating impingement jet
The objective of this study is to investigate the heat/mass transfer characteristics on various impinging jets under rotating condition. Two cooling schemes related to impingement jet are considered; array impingement jet cooling and impingement/effusion cooling. The test duct rotates at Ro = 0.075...
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Published in: | Applied thermal engineering 2009-10, Vol.29 (14), p.2914-2920 |
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container_end_page | 2920 |
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container_title | Applied thermal engineering |
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creator | Hong, Sung Kook Lee, Dong Hyun Cho, Hyung Hee |
description | The objective of this study is to investigate the heat/mass transfer characteristics on various impinging jets under rotating condition. Two cooling schemes related to impingement jet are considered; array impingement jet cooling and impingement/effusion cooling. The test duct rotates at Ro
=
0.075 with two different jet orientations and the jet Reynolds number is fixed at 5000. Two
H/
d configurations of 2.0 and 6.0 are conducted. The detailed heat/mass transfer coefficients on the target plate are measured by a naphthalene sublimation technique. The rotation changes the local heat/mass transfer characteristics due to the jet deflection and spreading phenomenon. For
H/
d
=
6.0, the jet is strongly deflected at the leading orientation, resulting in the significant decrease in heat/mass transfer. At the axial orientation, the momentum of jet core decreases slightly due to jet spreading into the radial direction and consequently, the value of stagnation peak is a little lower than that of the stationary case. However, reduction of heat/mass transfer due to rotation disappears at a low
H/
d of 2.0. In the averaged Sh, the leading orientation with
H/
d
=
6.0 shows 35% lower value than that of the stationary case whereas the other rotating cases lead to a similar value of the stationary case. |
doi_str_mv | 10.1016/j.applthermaleng.2009.02.014 |
format | article |
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=
0.075 with two different jet orientations and the jet Reynolds number is fixed at 5000. Two
H/
d configurations of 2.0 and 6.0 are conducted. The detailed heat/mass transfer coefficients on the target plate are measured by a naphthalene sublimation technique. The rotation changes the local heat/mass transfer characteristics due to the jet deflection and spreading phenomenon. For
H/
d
=
6.0, the jet is strongly deflected at the leading orientation, resulting in the significant decrease in heat/mass transfer. At the axial orientation, the momentum of jet core decreases slightly due to jet spreading into the radial direction and consequently, the value of stagnation peak is a little lower than that of the stationary case. However, reduction of heat/mass transfer due to rotation disappears at a low
H/
d of 2.0. In the averaged Sh, the leading orientation with
H/
d
=
6.0 shows 35% lower value than that of the stationary case whereas the other rotating cases lead to a similar value of the stationary case.</description><identifier>ISSN: 1359-4311</identifier><identifier>DOI: 10.1016/j.applthermaleng.2009.02.014</identifier><language>eng</language><publisher>Kidlington: Elsevier Ltd</publisher><subject>Applied sciences ; Coriolis force ; Energy ; Energy. Thermal use of fuels ; Engines and turbines ; Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc ; Exact sciences and technology ; Gas turbine ; Heat transfer ; Impingement jet ; Theoretical studies. Data and constants. Metering</subject><ispartof>Applied thermal engineering, 2009-10, Vol.29 (14), p.2914-2920</ispartof><rights>2009 Elsevier Ltd</rights><rights>2009 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c391t-32e84aee96048a9e0bc42413e7f9c786429f874ac6a7d355e378008b4b21d2ff3</citedby><cites>FETCH-LOGICAL-c391t-32e84aee96048a9e0bc42413e7f9c786429f874ac6a7d355e378008b4b21d2ff3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=21835761$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Hong, Sung Kook</creatorcontrib><creatorcontrib>Lee, Dong Hyun</creatorcontrib><creatorcontrib>Cho, Hyung Hee</creatorcontrib><title>Effect of jet direction on heat/mass transfer of rotating impingement jet</title><title>Applied thermal engineering</title><description>The objective of this study is to investigate the heat/mass transfer characteristics on various impinging jets under rotating condition. Two cooling schemes related to impingement jet are considered; array impingement jet cooling and impingement/effusion cooling. The test duct rotates at Ro
=
0.075 with two different jet orientations and the jet Reynolds number is fixed at 5000. Two
H/
d configurations of 2.0 and 6.0 are conducted. The detailed heat/mass transfer coefficients on the target plate are measured by a naphthalene sublimation technique. The rotation changes the local heat/mass transfer characteristics due to the jet deflection and spreading phenomenon. For
H/
d
=
6.0, the jet is strongly deflected at the leading orientation, resulting in the significant decrease in heat/mass transfer. At the axial orientation, the momentum of jet core decreases slightly due to jet spreading into the radial direction and consequently, the value of stagnation peak is a little lower than that of the stationary case. However, reduction of heat/mass transfer due to rotation disappears at a low
H/
d of 2.0. In the averaged Sh, the leading orientation with
H/
d
=
6.0 shows 35% lower value than that of the stationary case whereas the other rotating cases lead to a similar value of the stationary case.</description><subject>Applied sciences</subject><subject>Coriolis force</subject><subject>Energy</subject><subject>Energy. Thermal use of fuels</subject><subject>Engines and turbines</subject><subject>Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc</subject><subject>Exact sciences and technology</subject><subject>Gas turbine</subject><subject>Heat transfer</subject><subject>Impingement jet</subject><subject>Theoretical studies. Data and constants. Metering</subject><issn>1359-4311</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2009</creationdate><recordtype>article</recordtype><recordid>eNqNkEtLxDAQgHNQcF39Dz2ot3bzapuCF1l2VVjwoueQTSe7KX2ZZAX_vSldBG_CwDDwzetD6I7gjGBSrJpMjWMbjuA61UJ_yCjGVYZphgm_QAvC8irljJArdO19gzGhouQL9LoxBnRIBpM0EJLauljZoU9iHEGFVae8T4JTvTfgJswNQQXbHxLbjTFBB32Yem_QpVGth9tzXqKP7eZ9_ZLu3p5f10-7VLOKhJRREFwBVAXmQlWA95pTThiUptKlKDitTLxM6UKVNctzYKXAWOz5npKaGsOW6GGeO7rh8wQ-yM56DW2rehhOXjKei5yIIoKPM6jd4L0DI0dnO-W-JcFyciYb-deZnJxJTGV0Ftvvz3uU16o1UYG2_ncGJYLlZUEit505iE9_WXDSawu9htmlrAf7v4U_0Q2NNw</recordid><startdate>20091001</startdate><enddate>20091001</enddate><creator>Hong, Sung Kook</creator><creator>Lee, Dong Hyun</creator><creator>Cho, Hyung Hee</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>KR7</scope></search><sort><creationdate>20091001</creationdate><title>Effect of jet direction on heat/mass transfer of rotating impingement jet</title><author>Hong, Sung Kook ; Lee, Dong Hyun ; Cho, Hyung Hee</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c391t-32e84aee96048a9e0bc42413e7f9c786429f874ac6a7d355e378008b4b21d2ff3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2009</creationdate><topic>Applied sciences</topic><topic>Coriolis force</topic><topic>Energy</topic><topic>Energy. Thermal use of fuels</topic><topic>Engines and turbines</topic><topic>Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc</topic><topic>Exact sciences and technology</topic><topic>Gas turbine</topic><topic>Heat transfer</topic><topic>Impingement jet</topic><topic>Theoretical studies. Data and constants. Metering</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hong, Sung Kook</creatorcontrib><creatorcontrib>Lee, Dong Hyun</creatorcontrib><creatorcontrib>Cho, Hyung Hee</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>Civil Engineering Abstracts</collection><jtitle>Applied thermal engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Hong, Sung Kook</au><au>Lee, Dong Hyun</au><au>Cho, Hyung Hee</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Effect of jet direction on heat/mass transfer of rotating impingement jet</atitle><jtitle>Applied thermal engineering</jtitle><date>2009-10-01</date><risdate>2009</risdate><volume>29</volume><issue>14</issue><spage>2914</spage><epage>2920</epage><pages>2914-2920</pages><issn>1359-4311</issn><abstract>The objective of this study is to investigate the heat/mass transfer characteristics on various impinging jets under rotating condition. Two cooling schemes related to impingement jet are considered; array impingement jet cooling and impingement/effusion cooling. The test duct rotates at Ro
=
0.075 with two different jet orientations and the jet Reynolds number is fixed at 5000. Two
H/
d configurations of 2.0 and 6.0 are conducted. The detailed heat/mass transfer coefficients on the target plate are measured by a naphthalene sublimation technique. The rotation changes the local heat/mass transfer characteristics due to the jet deflection and spreading phenomenon. For
H/
d
=
6.0, the jet is strongly deflected at the leading orientation, resulting in the significant decrease in heat/mass transfer. At the axial orientation, the momentum of jet core decreases slightly due to jet spreading into the radial direction and consequently, the value of stagnation peak is a little lower than that of the stationary case. However, reduction of heat/mass transfer due to rotation disappears at a low
H/
d of 2.0. In the averaged Sh, the leading orientation with
H/
d
=
6.0 shows 35% lower value than that of the stationary case whereas the other rotating cases lead to a similar value of the stationary case.</abstract><cop>Kidlington</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.applthermaleng.2009.02.014</doi><tpages>7</tpages></addata></record> |
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source | Elsevier |
subjects | Applied sciences Coriolis force Energy Energy. Thermal use of fuels Engines and turbines Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc Exact sciences and technology Gas turbine Heat transfer Impingement jet Theoretical studies. Data and constants. Metering |
title | Effect of jet direction on heat/mass transfer of rotating impingement jet |
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