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Heat Transfer and Frictions in the Convergent/divergent Channel with Lambda/V-shaped Ribs on Two Walls

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dc.contributor.authorKim, Beom-soo-
dc.contributor.authorLee, Myung-sung-
dc.contributor.authorAhn, Soo-whan-
dc.date.accessioned2022-12-26T18:33:50Z-
dc.date.available2022-12-26T18:33:50Z-
dc.date.issued2017-09-
dc.identifier.issn2093-274X-
dc.identifier.issn2093-2480-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/13529-
dc.description.abstractThe local heat transfer and total pressure drops of developed turbulent flows in the ribbed rectangular convergent/divergent channels with Lambda/V-shaped ribs have been investigated experimentally. The channels have the exit hydraulic diameter (Dho) to inlet hydraulic diameter (D-ht) ratios of 0.67 for convergence and 1.49 for divergence, respectively. The Lambda/V-shaped ribs with three different flow attack angles of 30 degrees, 45 degrees, and 60 degrees are manufactured with a fixed rib height (e) of 10 mm and the ratio of rib spacing (S) to height (e) of 10 on the walls. Thermal performances of the ribbed rectangular convergent/divergent channels are compared with the smooth straight tube under identical pumping power. The results show that the flow attack angle of 45 degrees with.-shaped rib has the greatest thermal performance at all the Reynolds numbers studied in the convergent channel; whereas, the flow attack angle of 60 degrees with V-shaped rib has the greatest thermal performance over Reynolds number of 30,000 in the divergent channel.-
dc.format.extent8-
dc.language영어-
dc.language.isoENG-
dc.publisherSPRINGER-
dc.titleHeat Transfer and Frictions in the Convergent/divergent Channel with Lambda/V-shaped Ribs on Two Walls-
dc.typeArticle-
dc.publisher.location미국-
dc.identifier.doi10.5139/IJASS.2017.18.3.395-
dc.identifier.scopusid2-s2.0-85031815980-
dc.identifier.wosid000418886400002-
dc.identifier.bibliographicCitationINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.18, no.3, pp 395 - 402-
dc.citation.titleINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES-
dc.citation.volume18-
dc.citation.number3-
dc.citation.startPage395-
dc.citation.endPage402-
dc.type.docTypeArticle-
dc.identifier.kciidART002269952-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClassscie-
dc.description.journalRegisteredClassscopus-
dc.description.journalRegisteredClasskci-
dc.relation.journalResearchAreaEngineering-
dc.relation.journalWebOfScienceCategoryEngineering, Aerospace-
dc.subject.keywordAuthorRibbed rectangular convergent/divergent channel-
dc.subject.keywordAuthorLambda/V-shaped ribs-
dc.subject.keywordAuthorFlow attack angle-
dc.subject.keywordAuthorHeat transfer-
dc.subject.keywordAuthorTotal pressure drop-
dc.subject.keywordAuthorThermal performance-
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해양과학대학 > 기계시스템공학과 > Journal Articles

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해양과학대학 (기계시스템공학과)
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