DC Field | Value | Language |
---|---|---|
dc.contributor.author | Lee, J | - |
dc.contributor.author | Lee, SJ | - |
dc.date.accessioned | 2016-03-31T13:42:43Z | - |
dc.date.available | 2016-03-31T13:42:43Z | - |
dc.date.created | 2009-03-19 | - |
dc.date.issued | 1999-04 | - |
dc.identifier.issn | 0891-6152 | - |
dc.identifier.other | 1999-OAK-0000000707 | - |
dc.identifier.uri | https://oasis.postech.ac.kr/handle/2014.oak/20433 | - |
dc.description.abstract | The turbulent heat transfer characteristics in a stagnation region were investigated experimentally for an axisymmetric submerged air jet impinging normal to a heated flat plate. The temperature distribution on the heated flat surface was measured by a thermochromic liquid crystal (TLC) with digital image processing technique. To get precise heat transfer data inside the stagnation region, a fully developed straight pipe nozzle was used in this study. The stagnation Nusselt number was correlated for the jet Reynolds number and the nozzle-to-plate spacing as Nu(0) proportional to Re-0.565(L/D)(0.0384). For the nozzle-to-plate spacing of L/D = 2, the stagnation Nusselt number varies according to Nu(0) proportional to Re-0.50 and the local heat transfer rates exhibit two maxima. The primary and secondary maxima are attributed to the accelerated radial flow and the transition from a laminar to a turbulent boundary layer, respectively. For larger nozzle-to-plate spacings (L/D > 6), the local heat transfer decreases monotonically with radial distance. The Reynolds number dependence is enhanced as L/D increases (Nu(0) proportional to Re-0.58 for L/D = 6 and Nu(0) proportional to Re-0.65 for L/D = 10). This results from the increase of the centerline turbulent intensity of approaching jet due to strong momentum exchange with ambient fluids. | - |
dc.description.statementofresponsibility | X | - |
dc.language | English | - |
dc.publisher | TAYLOR & FRANCIS INC | - |
dc.relation.isPartOf | EXPERIMENTAL HEAT TRANSFER | - |
dc.subject | FLAT-PLATE | - |
dc.subject | AIR-JET | - |
dc.subject | VISUALIZATION | - |
dc.subject | GAS | - |
dc.title | Stagnation region heat transfer of a turbulent axisymmetric jet impingement | - |
dc.type | Article | - |
dc.contributor.college | 기계공학과 | - |
dc.identifier.doi | 10.1080/089161599269753 | - |
dc.author.google | Lee, J | - |
dc.author.google | Lee, SJ | - |
dc.relation.volume | 12 | - |
dc.relation.issue | 2 | - |
dc.relation.startpage | 137 | - |
dc.relation.lastpage | 156 | - |
dc.contributor.id | 10054593 | - |
dc.relation.journal | EXPERIMENTAL HEAT TRANSFER | - |
dc.relation.index | SCI급, SCOPUS 등재논문 | - |
dc.relation.sci | SCIE | - |
dc.collections.name | Journal Papers | - |
dc.type.rims | ART | - |
dc.identifier.bibliographicCitation | EXPERIMENTAL HEAT TRANSFER, v.12, no.2, pp.137 - 156 | - |
dc.identifier.wosid | 000079863700003 | - |
dc.date.tcdate | 2019-01-01 | - |
dc.citation.endPage | 156 | - |
dc.citation.number | 2 | - |
dc.citation.startPage | 137 | - |
dc.citation.title | EXPERIMENTAL HEAT TRANSFER | - |
dc.citation.volume | 12 | - |
dc.contributor.affiliatedAuthor | Lee, SJ | - |
dc.identifier.scopusid | 2-s2.0-0032648115 | - |
dc.description.journalClass | 1 | - |
dc.description.journalClass | 1 | - |
dc.description.wostc | 84 | - |
dc.type.docType | Article | - |
dc.subject.keywordPlus | FLAT-PLATE | - |
dc.subject.keywordPlus | AIR-JET | - |
dc.subject.keywordPlus | VISUALIZATION | - |
dc.subject.keywordPlus | GAS | - |
dc.relation.journalWebOfScienceCategory | Thermodynamics | - |
dc.relation.journalWebOfScienceCategory | Engineering, Mechanical | - |
dc.description.journalRegisteredClass | scie | - |
dc.description.journalRegisteredClass | scopus | - |
dc.relation.journalResearchArea | Thermodynamics | - |
dc.relation.journalResearchArea | Engineering | - |
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