The investigation of groove geometry effect on heat transfer for internally grooved tubes

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An experimental study of surface heat transfer and friction characteristics of a fully developed turbulent air flow in different grooved tubes is reported. Tests were performed for Reynolds number range 10,000-38,000 and for different geometric groove shapes (circular, trapezoidal and rectangular). The ratio of tube length-to-diameter is 33. Among the grooved tubes, heat transfer enhancement is obtained up to 63% for circular groove, 58% for trapezoidal groove and 47% for rectangular groove, in comparison with the smooth tube at the highest Reynolds number (Re = 38,000). Correlations of heat transfer and friction coefficient were obtained for different grooved tubes. In evaluation of thermal performance, it is seen that the grooved tubes are thermodynamically advantageous (Ns, a < 1) up to Re = 30,000 for circular and trapezoidal grooves and up to Re = 28,000 for rectangular grooves. It is observed that there is an optimum value of the entropy generation number at about Re = 17,000 for all investigated grooves. © 2008 Elsevier Ltd. All rights reserved.

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AlanDeğerDil
dc.contributor.authorBilen, Kadir
dc.contributor.authorCetin, Murat
dc.contributor.authorGul, Hasan
dc.contributor.authorBalta, Tuba
dc.date.accessioned2026-10-18T20:30:56.363515484Z
dc.date.available2026-10-18T20:30:56.363515484Z
dc.date.issued2009
dc.description.abstractAn experimental study of surface heat transfer and friction characteristics of a fully developed turbulent air flow in different grooved tubes is reported. Tests were performed for Reynolds number range 10,000-38,000 and for different geometric groove shapes (circular, trapezoidal and rectangular). The ratio of tube length-to-diameter is 33. Among the grooved tubes, heat transfer enhancement is obtained up to 63% for circular groove, 58% for trapezoidal groove and 47% for rectangular groove, in comparison with the smooth tube at the highest Reynolds number (Re = 38,000). Correlations of heat transfer and friction coefficient were obtained for different grooved tubes. In evaluation of thermal performance, it is seen that the grooved tubes are thermodynamically advantageous (Ns, a < 1) up to Re = 30,000 for circular and trapezoidal grooves and up to Re = 28,000 for rectangular grooves. It is observed that there is an optimum value of the entropy generation number at about Re = 17,000 for all investigated grooves. © 2008 Elsevier Ltd. All rights reserved.
dc.description.sponsorshipThis work was funded by the Ataturk University Research Foundation under 2001/157.
dc.identifier.doi10.1016/j.applthermaleng.2008.04.008
dc.identifier.endpage761
dc.identifier.issn1359-4311
dc.identifier.issue4
dc.identifier.scopus2-s2.0-56149092240
dc.identifier.startpage753
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/ebyu/16117
dc.identifier.volume29
dc.identifier.wosWOS:000264492500018
dc.language.isoen
dc.publisherPERGAMON-ELSEVIER SCIENCE LTD
dc.relation.ispartofApplied Thermal Engineering
dc.rightsinfo:eu-repo/semantics/openAccess
dc.subjectConvective heat transfer
dc.subjectGrooved tube
dc.subjectGrooves
dc.subjectHeat exchanger
dc.subjectHeat transfer enhancement/augmentation
dc.subjectRibs
dc.subjectAerodynamics
dc.subjectAir
dc.subjectFriction
dc.subjectHeat exchangers
dc.subjectHeat transfer
dc.subjectHeating equipment
dc.subjectMixed convection
dc.subjectReynolds number
dc.subjectRhenium
dc.subjectThermoanalysis
dc.subjectAir flows
dc.subjectCircular grooves
dc.subjectEntropy generations
dc.subjectExperimental studies
dc.subjectFriction characteristics
dc.subjectFriction coefficients
dc.subjectGroove geometries
dc.subjectGroove shapes
dc.subjectGrooved tubes
dc.subjectHeat Transfer enhancements
dc.subjectOptimum values
dc.subjectRectangular grooves
dc.subjectSmooth tubes
dc.subjectSurface heat transfers
dc.titleThe investigation of groove geometry effect on heat transfer for internally grooved tubes
dc.typeArticle
dspace.entity.typePublication
rdl.citation.scopus236
rdl.citation.wos207
rdl.source.indexSCOPUS
rdl.source.indexWOS
rdl.wos.indexScience Citation Index Expanded (SCI-EXPANDED)