Açık Akademik Arşiv Sistemi

Jet impingement cooling on a rib-roughened surface using extended jet holes

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dc.date.accessioned 2021-06-08T09:11:50Z
dc.date.available 2021-06-08T09:11:50Z
dc.date.issued 2020
dc.identifier.issn 1359-4311
dc.identifier.uri https://hdl.handle.net/20.500.12619/96110
dc.description This work was supported by the Scientific and Technological Research Council of Turkey (TUBITAK, PN: 118M795).
dc.description Bu yayının lisans anlaşması koşulları tam metin açık erişimine izin vermemektedir.
dc.description.abstract In this study, jet impingement cooling on a rib-roughened surface has been investigated experimentally. The aim of this study is to investigate the effect of extended jet holes on the heat transfer performance and flow characteristics of the jet impingement cooling on a rib-roughened surface. The studies have been conducted under turbulent flow condition (16,250 <= Re-j <= 32,500). Transient Liquid Crystals (TLC) method has been employed to investigate the average and local Nusselt number (Nu) distributions on the surface of interest. Six inline arrays of jet impingement configuration have been examined as the jet impingement cooling system. Jet holes were extended towards the target surface with the nozzles. Various dimensionless nozzles to the target surface gaps (G(j)/D-j = 1.0, 2.0, 3.0, 4.0 and 5.0) have been investigated. Rectangular cross-sectional ribs were located on the surface of interest for the augmentation of heat transfer. Experimental studies were conducted on the dimensionless rib height as H-r/D-j = 0.42. In addition, numerical studies were carried out to investigate the flow and heat transfer characteristics. The effect of various dimensionless rib heights (H-r/D-j) on convective heat transfer performance has also been investigated numerically. SST k-omega with low-Re correction turbulence model was used for solving turbulence equations. Average and local Nu number distributions, flow characteristics and Performance Evaluation Criterion (PEC) were examined in detail. Results were compared with the orifice plate (G(j)/D-j = 6.0) jet impingement configuration. Results showed that SST k-omega turbulence model accurately reveals the experimental data. Application of extended jet holes is a feasible method for practical application of the jet impingement cooling, especially at relatively low dimensionless nozzle gap (G(j)/D-j <= 4.0). Furthermore, improperly designed rib height has been found to diminish heat transfer performance.
dc.description.sponsorship Scientific and Technological Research Council of Turkey (TUBITAK)Turkiye Bilimsel ve Teknolojik Arastirma Kurumu (TUBITAK) [PN: 118M795]
dc.language English
dc.language.iso eng
dc.publisher PERGAMON-ELSEVIER SCIENCE LTD
dc.relation.isversionof 10.1016/j.applthermaleng.2020.115601
dc.rights info:eu-repo/semantics/closedAccess
dc.subject HEAT-TRANSFER CHARACTERISTICS
dc.subject NUMERICAL INVESTIGATIONS
dc.subject FLOW
dc.subject FLAT
dc.subject WALL
dc.subject DUCT
dc.title Jet impingement cooling on a rib-roughened surface using extended jet holes
dc.type Article
dc.contributor.authorID TEPE, Ahmet Umit/0000-0001-7626-6348
dc.contributor.authorID ARSLAN, Kamil/0000-0002-1216-6812
dc.identifier.volume 178
dc.relation.journal APPLIED THERMAL ENGINEERING
dc.identifier.doi 10.1016/j.applthermaleng.2020.115601
dc.identifier.eissn 1873-5606
dc.contributor.author Tepe, Ahmet Umit
dc.contributor.author Uysal, Unal
dc.contributor.author Yetisken, Yasar
dc.contributor.author Arslan, Kamil
dc.relation.publicationcategory Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı


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