Experimental investigation of the thermal performance effects of turbulators with different fin angles in a circular pipe

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In this study, we experimentally investigated the heat transmission and friction effects of finned turbulators with different angles in a circular pipe for single-phase flows. Experiments were conducted to see how turbulators affected the friction factor and Nusselt number. The Nusselt numbers of the finned turbulators with 30°, 20° and 10° angles rose by 121.66%, 109.05% and 81.30%, respectively, in comparison to the plain pipe, according to experiments using Reynolds numbers in the range of 10043-14386. The overall heat transfer improvement of all turbulator types appears to be more than one. Due to the increase in blade angle, the highest Nu number was obtained from the experiment with a 30° angle fin turbulator, but the greatest heat transfer improvement was obtained as 1.476 in a 20° angle blade turbulator for Re = 10043 number. The thermal improvement factors of 20° and 30° angle fin turbulators were found to be 1.1 and 1.07 times more than, respectively, compared to the turbulator with a 10° angle. In addition, it has been shown that the 20° angle fin turbulator's thermal improvement factor is 1.03 times higher than the 30° angle turbulator's. © 2022 Elsevier Masson SAS

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RDL Kalıcı Bağlantı (PID)
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dc.contributor.authorFirat, Ilker
dc.contributor.authorKaragoz, Sendogan
dc.contributor.authorYildirim, Orhan
dc.contributor.authorSonmez, Fatin
dc.date.accessioned2026-10-18T20:27:06.630505512Z
dc.date.available2026-10-18T20:27:06.630505512Z
dc.date.issued2023
dc.description.abstractIn this study, we experimentally investigated the heat transmission and friction effects of finned turbulators with different angles in a circular pipe for single-phase flows. Experiments were conducted to see how turbulators affected the friction factor and Nusselt number. The Nusselt numbers of the finned turbulators with 30°, 20° and 10° angles rose by 121.66%, 109.05% and 81.30%, respectively, in comparison to the plain pipe, according to experiments using Reynolds numbers in the range of 10043-14386. The overall heat transfer improvement of all turbulator types appears to be more than one. Due to the increase in blade angle, the highest Nu number was obtained from the experiment with a 30° angle fin turbulator, but the greatest heat transfer improvement was obtained as 1.476 in a 20° angle blade turbulator for Re = 10043 number. The thermal improvement factors of 20° and 30° angle fin turbulators were found to be 1.1 and 1.07 times more than, respectively, compared to the turbulator with a 10° angle. In addition, it has been shown that the 20° angle fin turbulator's thermal improvement factor is 1.03 times higher than the 30° angle turbulator's. © 2022 Elsevier Masson SAS
dc.identifier.doi10.1016/j.ijthermalsci.2022.107969
dc.identifier.eissn1778-4166
dc.identifier.issn1290-0729
dc.identifier.scopus2-s2.0-85140229923
dc.identifier.startpage107969
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/ebyu/12176
dc.identifier.volume184
dc.identifier.wosWOS:000882358300003
dc.language.isoen
dc.publisherElsevier Masson s.r.l.
dc.relation.ispartofInternational Journal of Thermal Sciences
dc.rightsinfo:eu-repo/semantics/openAccess
dc.subjectFriction factor
dc.subjectHeat transfer
dc.subjectPressure drop
dc.subjectTurbulator
dc.subjectTurbulent flow
dc.subjectFins (heat exchange)
dc.subjectFriction
dc.subjectReynolds number
dc.subjectCircular pipe
dc.subjectExperimental investigations
dc.subjectFriction factors
dc.subjectHeat frictions
dc.subjectHeat transmission
dc.subjectImprovement factors
dc.subjectPerformance effect
dc.subjectThermal
dc.subjectThermal Performance
dc.subjectTurbulators
dc.subjectNusselt number
dc.titleExperimental investigation of the thermal performance effects of turbulators with different fin angles in a circular pipe
dc.typeArticle
dspace.entity.typePublication
rdl.citation.scopus28
rdl.citation.wos28
rdl.source.indexSCOPUS
rdl.source.indexWOS
rdl.wos.indexScience Citation Index Expanded (SCI-EXPANDED)