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Heat Transfer and Frictions in the Convergent/divergent Channel with Lambda/V-shaped Ribs on Two Walls
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Kim, Beom-soo | - |
| dc.contributor.author | Lee, Myung-sung | - |
| dc.contributor.author | Ahn, Soo-whan | - |
| dc.date.accessioned | 2022-12-26T18:33:50Z | - |
| dc.date.available | 2022-12-26T18:33:50Z | - |
| dc.date.issued | 2017-09 | - |
| dc.identifier.issn | 2093-274X | - |
| dc.identifier.issn | 2093-2480 | - |
| dc.identifier.uri | https://scholarworks.gnu.ac.kr/handle/sw.gnu/13529 | - |
| dc.description.abstract | The 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.extent | 8 | - |
| dc.language | 영어 | - |
| dc.language.iso | ENG | - |
| dc.publisher | SPRINGER | - |
| dc.title | Heat Transfer and Frictions in the Convergent/divergent Channel with Lambda/V-shaped Ribs on Two Walls | - |
| dc.type | Article | - |
| dc.publisher.location | 미국 | - |
| dc.identifier.doi | 10.5139/IJASS.2017.18.3.395 | - |
| dc.identifier.scopusid | 2-s2.0-85031815980 | - |
| dc.identifier.wosid | 000418886400002 | - |
| dc.identifier.bibliographicCitation | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.18, no.3, pp 395 - 402 | - |
| dc.citation.title | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES | - |
| dc.citation.volume | 18 | - |
| dc.citation.number | 3 | - |
| dc.citation.startPage | 395 | - |
| dc.citation.endPage | 402 | - |
| dc.type.docType | Article | - |
| dc.identifier.kciid | ART002269952 | - |
| dc.description.isOpenAccess | N | - |
| dc.description.journalRegisteredClass | scie | - |
| dc.description.journalRegisteredClass | scopus | - |
| dc.description.journalRegisteredClass | kci | - |
| dc.relation.journalResearchArea | Engineering | - |
| dc.relation.journalWebOfScienceCategory | Engineering, Aerospace | - |
| dc.subject.keywordAuthor | Ribbed rectangular convergent/divergent channel | - |
| dc.subject.keywordAuthor | Lambda/V-shaped ribs | - |
| dc.subject.keywordAuthor | Flow attack angle | - |
| dc.subject.keywordAuthor | Heat transfer | - |
| dc.subject.keywordAuthor | Total pressure drop | - |
| dc.subject.keywordAuthor | Thermal performance | - |
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